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7/21/2019 l11 Interface http://slidepdf.com/reader/full/l11-interface 1/25 Copyright 2005 ABAQUS, Inc. ABAQUS/Explicit: Advanced Topics ABAQUS/Explicit–ABAQUS/Standard Interface Lecture 11 Copyright 2005 ABAQUS, Inc. ABAQUS/Explicit: Advanced Topics L11.2 Overview Introduction Import from ABAQUS/Explicit to ABAQUS/Standard Import from ABAQUS/Standard to ABAQUS/Explicit Additional Import Modeling Issues Limitations Demonstration

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Page 1: l11 Interface

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

ABAQUSExplicitndashABAQUSStandard

Interface

Lecture 11

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L112

Overview

bull Introduction

bull Import from ABAQUSExplicit to ABAQUSStandard

bull Import from ABAQUSStandard to ABAQUSExplicit

bull Additional Import Modeling Issues

bull Limitations

bull Demonstration

7212019 l11 Interface

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Introduction

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L114

Introduction

bull ABAQUS provides a capability to transfer a deformed mesh and

associated state between an ABAQUSExplicit analysis and an

ABAQUSStandard analysis

ABAQUSStandard

ABAQUSExplicit

ABAQUSStandard

ABAQUSExplicit

ABAQUSStandard

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L115

Introduction

ndash The deformed model can be transferred from ABAQUSExplicit to

ABAQUSStandard to

bull Obtain the final static configuration after a dynamic event

bull Simulate springback

bull Perform eigenvalue or buckling simulations on the formed part

Two-dimensional draw bending forming and springback analysis

Blank after forming (ABAQUSExplicit )

Springback (ABAQUSStandard )Initial assembly for forming process

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L116

Introduction

ndash The deformed model can be transferred from ABAQUSStandard to

ABAQUSExplicit to

bull Simulate a preloading phase where the capabilities of

ABAQUSExplicit are not needed (no contact etc)

bull Simulate further forming steps after an intermediary springback phase

bull Simulate a transient event after steady-state conditions have beenfound (eg with a steady-state transport simulation)

Tire footprint and steady-state rolling

(ABAQUSStandard)

Tire hitting curb

(ABAQUSExplicit)

Import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L117

Introduction

bull Summary of import capabilities

Fluid elements Amplitude definitions

Infinite elementsNodal transformationsRebar layers

Mass and rotary inertia elementsKinematic constraintsTemperatures

Dashpot and spring elementsOutput requestsNodes node sets

Connector elementsContact definitionsElements element sets

Mesh-independent fastenersLoadsNodal positions

Analytical rigid surfacesBoundary conditionsMaterial state

Cannot be importedNeed to be respecifiedCan be imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSExplicit to

ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L119

Import from ABAQUSExplicit to ABAQUSStandard

bull The following example demonstrates the procedure for transferring

results from ABAQUSExplicit to ABAQUSStandard

Initial mesh of deformable blank and rigid

tools One-quarter of the box is modeled

bull Example Deep drawing of a square box

ndash The blank undergoes large

deformations during the sheet metalforming process

ndash Once the forming process is complete

and the confining tools are removed

the blank will attempt to recover its

elastic deformation

ndash This springback phenomenon may

lead to unacceptable warping of theformed product

bull Forming tools must be designed

to compensate for springback

effects

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1110

Import from ABAQUSExplicit to ABAQUSStandard

ndash For the calculation of springback associated with the sheet metal forming

processes

bull The forming process is simulated using ABAQUSExplicit

bull The deformed mesh of the blank and its associated state at the end ofthe forming process are imported into ABAQUSStandard

bull The springback calculation is performed in ABAQUSStandard

ndash The displacement field that ABAQUSStandard calculates is the

amount of springback that occurs provided that the reference

configuration is updated

bull If it is not the displacements will be total values including theforming phases

1

2

3

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1111

Import from ABAQUSExplicit to ABAQUSStandard

bull The forming process is simulated using ABAQUSExplicit

ndash During the analysis restart data must be written at the time when transfer of

the modelrsquos state is required (ie at the end of the forming analysis)

ndash The ABAQUSExplicit analysis will produce the following files which will be

used to import the final deformed shape of the blank into ABAQUSStandard

bull State (abq )

bull Analysis database (stt and pac)

bull Part (prt) and

bull Output database (odb) files

RESTART WRITE NUMBER INTERVAL=1

1

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1112

Import from ABAQUSExplicit to ABAQUSStandard

ndash Results at the end of the ABAQUSExplicit forming analysis

Mises stress contours for the bottom surface of the blank

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1113

Import from ABAQUSExplicit to ABAQUSStandard

bull The deformed mesh of the blank and its associated state at the end of the

forming process are imported into ABAQUSStandard

2

Copy the forming model into a

new modela a

ABAQUSCAE interface Keywords interface

In a text editor and begin a new

input file

HEADING

Springback Calculation

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1114

Import from ABAQUSExplicit to ABAQUSStandard

Replace (and rename) the dynamic ABAQUSExplicit

step with a static ABAQUSStandard step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

b b Define an ABAQUSStandard

static step

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1115

Import from ABAQUSExplicit to ABAQUSStandard

Keep blank and associated sets boundary conditions etc

ABAQUSCAE interface only

c1 Delete interactions rigid tools and associated sets

boundary conditions etc

c2

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1116

Import from ABAQUSExplicit to ABAQUSStandard

Define an initial state field to import forming

analysis results for the blank part instance

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d1 d1 Import element set BLANK from the

forming analysis

BLANK was the element set used for the blank section

definition in the original forming analysis

SHELL SECTION ELSET=BLANK

a requirement for input files not defined as

assemblies of part instances

In ABAQUSCAE and input files defined using parts

and assemblies part instances are specified for

import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Introduction

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L114

Introduction

bull ABAQUS provides a capability to transfer a deformed mesh and

associated state between an ABAQUSExplicit analysis and an

ABAQUSStandard analysis

ABAQUSStandard

ABAQUSExplicit

ABAQUSStandard

ABAQUSExplicit

ABAQUSStandard

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L115

Introduction

ndash The deformed model can be transferred from ABAQUSExplicit to

ABAQUSStandard to

bull Obtain the final static configuration after a dynamic event

bull Simulate springback

bull Perform eigenvalue or buckling simulations on the formed part

Two-dimensional draw bending forming and springback analysis

Blank after forming (ABAQUSExplicit )

Springback (ABAQUSStandard )Initial assembly for forming process

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L116

Introduction

ndash The deformed model can be transferred from ABAQUSStandard to

ABAQUSExplicit to

bull Simulate a preloading phase where the capabilities of

ABAQUSExplicit are not needed (no contact etc)

bull Simulate further forming steps after an intermediary springback phase

bull Simulate a transient event after steady-state conditions have beenfound (eg with a steady-state transport simulation)

Tire footprint and steady-state rolling

(ABAQUSStandard)

Tire hitting curb

(ABAQUSExplicit)

Import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L117

Introduction

bull Summary of import capabilities

Fluid elements Amplitude definitions

Infinite elementsNodal transformationsRebar layers

Mass and rotary inertia elementsKinematic constraintsTemperatures

Dashpot and spring elementsOutput requestsNodes node sets

Connector elementsContact definitionsElements element sets

Mesh-independent fastenersLoadsNodal positions

Analytical rigid surfacesBoundary conditionsMaterial state

Cannot be importedNeed to be respecifiedCan be imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSExplicit to

ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L119

Import from ABAQUSExplicit to ABAQUSStandard

bull The following example demonstrates the procedure for transferring

results from ABAQUSExplicit to ABAQUSStandard

Initial mesh of deformable blank and rigid

tools One-quarter of the box is modeled

bull Example Deep drawing of a square box

ndash The blank undergoes large

deformations during the sheet metalforming process

ndash Once the forming process is complete

and the confining tools are removed

the blank will attempt to recover its

elastic deformation

ndash This springback phenomenon may

lead to unacceptable warping of theformed product

bull Forming tools must be designed

to compensate for springback

effects

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1110

Import from ABAQUSExplicit to ABAQUSStandard

ndash For the calculation of springback associated with the sheet metal forming

processes

bull The forming process is simulated using ABAQUSExplicit

bull The deformed mesh of the blank and its associated state at the end ofthe forming process are imported into ABAQUSStandard

bull The springback calculation is performed in ABAQUSStandard

ndash The displacement field that ABAQUSStandard calculates is the

amount of springback that occurs provided that the reference

configuration is updated

bull If it is not the displacements will be total values including theforming phases

1

2

3

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1111

Import from ABAQUSExplicit to ABAQUSStandard

bull The forming process is simulated using ABAQUSExplicit

ndash During the analysis restart data must be written at the time when transfer of

the modelrsquos state is required (ie at the end of the forming analysis)

ndash The ABAQUSExplicit analysis will produce the following files which will be

used to import the final deformed shape of the blank into ABAQUSStandard

bull State (abq )

bull Analysis database (stt and pac)

bull Part (prt) and

bull Output database (odb) files

RESTART WRITE NUMBER INTERVAL=1

1

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1112

Import from ABAQUSExplicit to ABAQUSStandard

ndash Results at the end of the ABAQUSExplicit forming analysis

Mises stress contours for the bottom surface of the blank

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1113

Import from ABAQUSExplicit to ABAQUSStandard

bull The deformed mesh of the blank and its associated state at the end of the

forming process are imported into ABAQUSStandard

2

Copy the forming model into a

new modela a

ABAQUSCAE interface Keywords interface

In a text editor and begin a new

input file

HEADING

Springback Calculation

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1114

Import from ABAQUSExplicit to ABAQUSStandard

Replace (and rename) the dynamic ABAQUSExplicit

step with a static ABAQUSStandard step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

b b Define an ABAQUSStandard

static step

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1115

Import from ABAQUSExplicit to ABAQUSStandard

Keep blank and associated sets boundary conditions etc

ABAQUSCAE interface only

c1 Delete interactions rigid tools and associated sets

boundary conditions etc

c2

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1116

Import from ABAQUSExplicit to ABAQUSStandard

Define an initial state field to import forming

analysis results for the blank part instance

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d1 d1 Import element set BLANK from the

forming analysis

BLANK was the element set used for the blank section

definition in the original forming analysis

SHELL SECTION ELSET=BLANK

a requirement for input files not defined as

assemblies of part instances

In ABAQUSCAE and input files defined using parts

and assemblies part instances are specified for

import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 3: l11 Interface

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L115

Introduction

ndash The deformed model can be transferred from ABAQUSExplicit to

ABAQUSStandard to

bull Obtain the final static configuration after a dynamic event

bull Simulate springback

bull Perform eigenvalue or buckling simulations on the formed part

Two-dimensional draw bending forming and springback analysis

Blank after forming (ABAQUSExplicit )

Springback (ABAQUSStandard )Initial assembly for forming process

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L116

Introduction

ndash The deformed model can be transferred from ABAQUSStandard to

ABAQUSExplicit to

bull Simulate a preloading phase where the capabilities of

ABAQUSExplicit are not needed (no contact etc)

bull Simulate further forming steps after an intermediary springback phase

bull Simulate a transient event after steady-state conditions have beenfound (eg with a steady-state transport simulation)

Tire footprint and steady-state rolling

(ABAQUSStandard)

Tire hitting curb

(ABAQUSExplicit)

Import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L117

Introduction

bull Summary of import capabilities

Fluid elements Amplitude definitions

Infinite elementsNodal transformationsRebar layers

Mass and rotary inertia elementsKinematic constraintsTemperatures

Dashpot and spring elementsOutput requestsNodes node sets

Connector elementsContact definitionsElements element sets

Mesh-independent fastenersLoadsNodal positions

Analytical rigid surfacesBoundary conditionsMaterial state

Cannot be importedNeed to be respecifiedCan be imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSExplicit to

ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L119

Import from ABAQUSExplicit to ABAQUSStandard

bull The following example demonstrates the procedure for transferring

results from ABAQUSExplicit to ABAQUSStandard

Initial mesh of deformable blank and rigid

tools One-quarter of the box is modeled

bull Example Deep drawing of a square box

ndash The blank undergoes large

deformations during the sheet metalforming process

ndash Once the forming process is complete

and the confining tools are removed

the blank will attempt to recover its

elastic deformation

ndash This springback phenomenon may

lead to unacceptable warping of theformed product

bull Forming tools must be designed

to compensate for springback

effects

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1110

Import from ABAQUSExplicit to ABAQUSStandard

ndash For the calculation of springback associated with the sheet metal forming

processes

bull The forming process is simulated using ABAQUSExplicit

bull The deformed mesh of the blank and its associated state at the end ofthe forming process are imported into ABAQUSStandard

bull The springback calculation is performed in ABAQUSStandard

ndash The displacement field that ABAQUSStandard calculates is the

amount of springback that occurs provided that the reference

configuration is updated

bull If it is not the displacements will be total values including theforming phases

1

2

3

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1111

Import from ABAQUSExplicit to ABAQUSStandard

bull The forming process is simulated using ABAQUSExplicit

ndash During the analysis restart data must be written at the time when transfer of

the modelrsquos state is required (ie at the end of the forming analysis)

ndash The ABAQUSExplicit analysis will produce the following files which will be

used to import the final deformed shape of the blank into ABAQUSStandard

bull State (abq )

bull Analysis database (stt and pac)

bull Part (prt) and

bull Output database (odb) files

RESTART WRITE NUMBER INTERVAL=1

1

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1112

Import from ABAQUSExplicit to ABAQUSStandard

ndash Results at the end of the ABAQUSExplicit forming analysis

Mises stress contours for the bottom surface of the blank

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1113

Import from ABAQUSExplicit to ABAQUSStandard

bull The deformed mesh of the blank and its associated state at the end of the

forming process are imported into ABAQUSStandard

2

Copy the forming model into a

new modela a

ABAQUSCAE interface Keywords interface

In a text editor and begin a new

input file

HEADING

Springback Calculation

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1114

Import from ABAQUSExplicit to ABAQUSStandard

Replace (and rename) the dynamic ABAQUSExplicit

step with a static ABAQUSStandard step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

b b Define an ABAQUSStandard

static step

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1115

Import from ABAQUSExplicit to ABAQUSStandard

Keep blank and associated sets boundary conditions etc

ABAQUSCAE interface only

c1 Delete interactions rigid tools and associated sets

boundary conditions etc

c2

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1116

Import from ABAQUSExplicit to ABAQUSStandard

Define an initial state field to import forming

analysis results for the blank part instance

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d1 d1 Import element set BLANK from the

forming analysis

BLANK was the element set used for the blank section

definition in the original forming analysis

SHELL SECTION ELSET=BLANK

a requirement for input files not defined as

assemblies of part instances

In ABAQUSCAE and input files defined using parts

and assemblies part instances are specified for

import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 4: l11 Interface

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L117

Introduction

bull Summary of import capabilities

Fluid elements Amplitude definitions

Infinite elementsNodal transformationsRebar layers

Mass and rotary inertia elementsKinematic constraintsTemperatures

Dashpot and spring elementsOutput requestsNodes node sets

Connector elementsContact definitionsElements element sets

Mesh-independent fastenersLoadsNodal positions

Analytical rigid surfacesBoundary conditionsMaterial state

Cannot be importedNeed to be respecifiedCan be imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSExplicit to

ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L119

Import from ABAQUSExplicit to ABAQUSStandard

bull The following example demonstrates the procedure for transferring

results from ABAQUSExplicit to ABAQUSStandard

Initial mesh of deformable blank and rigid

tools One-quarter of the box is modeled

bull Example Deep drawing of a square box

ndash The blank undergoes large

deformations during the sheet metalforming process

ndash Once the forming process is complete

and the confining tools are removed

the blank will attempt to recover its

elastic deformation

ndash This springback phenomenon may

lead to unacceptable warping of theformed product

bull Forming tools must be designed

to compensate for springback

effects

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1110

Import from ABAQUSExplicit to ABAQUSStandard

ndash For the calculation of springback associated with the sheet metal forming

processes

bull The forming process is simulated using ABAQUSExplicit

bull The deformed mesh of the blank and its associated state at the end ofthe forming process are imported into ABAQUSStandard

bull The springback calculation is performed in ABAQUSStandard

ndash The displacement field that ABAQUSStandard calculates is the

amount of springback that occurs provided that the reference

configuration is updated

bull If it is not the displacements will be total values including theforming phases

1

2

3

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1111

Import from ABAQUSExplicit to ABAQUSStandard

bull The forming process is simulated using ABAQUSExplicit

ndash During the analysis restart data must be written at the time when transfer of

the modelrsquos state is required (ie at the end of the forming analysis)

ndash The ABAQUSExplicit analysis will produce the following files which will be

used to import the final deformed shape of the blank into ABAQUSStandard

bull State (abq )

bull Analysis database (stt and pac)

bull Part (prt) and

bull Output database (odb) files

RESTART WRITE NUMBER INTERVAL=1

1

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1112

Import from ABAQUSExplicit to ABAQUSStandard

ndash Results at the end of the ABAQUSExplicit forming analysis

Mises stress contours for the bottom surface of the blank

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1113

Import from ABAQUSExplicit to ABAQUSStandard

bull The deformed mesh of the blank and its associated state at the end of the

forming process are imported into ABAQUSStandard

2

Copy the forming model into a

new modela a

ABAQUSCAE interface Keywords interface

In a text editor and begin a new

input file

HEADING

Springback Calculation

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1114

Import from ABAQUSExplicit to ABAQUSStandard

Replace (and rename) the dynamic ABAQUSExplicit

step with a static ABAQUSStandard step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

b b Define an ABAQUSStandard

static step

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1115

Import from ABAQUSExplicit to ABAQUSStandard

Keep blank and associated sets boundary conditions etc

ABAQUSCAE interface only

c1 Delete interactions rigid tools and associated sets

boundary conditions etc

c2

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1116

Import from ABAQUSExplicit to ABAQUSStandard

Define an initial state field to import forming

analysis results for the blank part instance

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d1 d1 Import element set BLANK from the

forming analysis

BLANK was the element set used for the blank section

definition in the original forming analysis

SHELL SECTION ELSET=BLANK

a requirement for input files not defined as

assemblies of part instances

In ABAQUSCAE and input files defined using parts

and assemblies part instances are specified for

import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L119

Import from ABAQUSExplicit to ABAQUSStandard

bull The following example demonstrates the procedure for transferring

results from ABAQUSExplicit to ABAQUSStandard

Initial mesh of deformable blank and rigid

tools One-quarter of the box is modeled

bull Example Deep drawing of a square box

ndash The blank undergoes large

deformations during the sheet metalforming process

ndash Once the forming process is complete

and the confining tools are removed

the blank will attempt to recover its

elastic deformation

ndash This springback phenomenon may

lead to unacceptable warping of theformed product

bull Forming tools must be designed

to compensate for springback

effects

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1110

Import from ABAQUSExplicit to ABAQUSStandard

ndash For the calculation of springback associated with the sheet metal forming

processes

bull The forming process is simulated using ABAQUSExplicit

bull The deformed mesh of the blank and its associated state at the end ofthe forming process are imported into ABAQUSStandard

bull The springback calculation is performed in ABAQUSStandard

ndash The displacement field that ABAQUSStandard calculates is the

amount of springback that occurs provided that the reference

configuration is updated

bull If it is not the displacements will be total values including theforming phases

1

2

3

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1111

Import from ABAQUSExplicit to ABAQUSStandard

bull The forming process is simulated using ABAQUSExplicit

ndash During the analysis restart data must be written at the time when transfer of

the modelrsquos state is required (ie at the end of the forming analysis)

ndash The ABAQUSExplicit analysis will produce the following files which will be

used to import the final deformed shape of the blank into ABAQUSStandard

bull State (abq )

bull Analysis database (stt and pac)

bull Part (prt) and

bull Output database (odb) files

RESTART WRITE NUMBER INTERVAL=1

1

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1112

Import from ABAQUSExplicit to ABAQUSStandard

ndash Results at the end of the ABAQUSExplicit forming analysis

Mises stress contours for the bottom surface of the blank

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1113

Import from ABAQUSExplicit to ABAQUSStandard

bull The deformed mesh of the blank and its associated state at the end of the

forming process are imported into ABAQUSStandard

2

Copy the forming model into a

new modela a

ABAQUSCAE interface Keywords interface

In a text editor and begin a new

input file

HEADING

Springback Calculation

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1114

Import from ABAQUSExplicit to ABAQUSStandard

Replace (and rename) the dynamic ABAQUSExplicit

step with a static ABAQUSStandard step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

b b Define an ABAQUSStandard

static step

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1115

Import from ABAQUSExplicit to ABAQUSStandard

Keep blank and associated sets boundary conditions etc

ABAQUSCAE interface only

c1 Delete interactions rigid tools and associated sets

boundary conditions etc

c2

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1116

Import from ABAQUSExplicit to ABAQUSStandard

Define an initial state field to import forming

analysis results for the blank part instance

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d1 d1 Import element set BLANK from the

forming analysis

BLANK was the element set used for the blank section

definition in the original forming analysis

SHELL SECTION ELSET=BLANK

a requirement for input files not defined as

assemblies of part instances

In ABAQUSCAE and input files defined using parts

and assemblies part instances are specified for

import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1111

Import from ABAQUSExplicit to ABAQUSStandard

bull The forming process is simulated using ABAQUSExplicit

ndash During the analysis restart data must be written at the time when transfer of

the modelrsquos state is required (ie at the end of the forming analysis)

ndash The ABAQUSExplicit analysis will produce the following files which will be

used to import the final deformed shape of the blank into ABAQUSStandard

bull State (abq )

bull Analysis database (stt and pac)

bull Part (prt) and

bull Output database (odb) files

RESTART WRITE NUMBER INTERVAL=1

1

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1112

Import from ABAQUSExplicit to ABAQUSStandard

ndash Results at the end of the ABAQUSExplicit forming analysis

Mises stress contours for the bottom surface of the blank

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1113

Import from ABAQUSExplicit to ABAQUSStandard

bull The deformed mesh of the blank and its associated state at the end of the

forming process are imported into ABAQUSStandard

2

Copy the forming model into a

new modela a

ABAQUSCAE interface Keywords interface

In a text editor and begin a new

input file

HEADING

Springback Calculation

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1114

Import from ABAQUSExplicit to ABAQUSStandard

Replace (and rename) the dynamic ABAQUSExplicit

step with a static ABAQUSStandard step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

b b Define an ABAQUSStandard

static step

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1115

Import from ABAQUSExplicit to ABAQUSStandard

Keep blank and associated sets boundary conditions etc

ABAQUSCAE interface only

c1 Delete interactions rigid tools and associated sets

boundary conditions etc

c2

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1116

Import from ABAQUSExplicit to ABAQUSStandard

Define an initial state field to import forming

analysis results for the blank part instance

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d1 d1 Import element set BLANK from the

forming analysis

BLANK was the element set used for the blank section

definition in the original forming analysis

SHELL SECTION ELSET=BLANK

a requirement for input files not defined as

assemblies of part instances

In ABAQUSCAE and input files defined using parts

and assemblies part instances are specified for

import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1113

Import from ABAQUSExplicit to ABAQUSStandard

bull The deformed mesh of the blank and its associated state at the end of the

forming process are imported into ABAQUSStandard

2

Copy the forming model into a

new modela a

ABAQUSCAE interface Keywords interface

In a text editor and begin a new

input file

HEADING

Springback Calculation

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1114

Import from ABAQUSExplicit to ABAQUSStandard

Replace (and rename) the dynamic ABAQUSExplicit

step with a static ABAQUSStandard step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

b b Define an ABAQUSStandard

static step

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1115

Import from ABAQUSExplicit to ABAQUSStandard

Keep blank and associated sets boundary conditions etc

ABAQUSCAE interface only

c1 Delete interactions rigid tools and associated sets

boundary conditions etc

c2

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1116

Import from ABAQUSExplicit to ABAQUSStandard

Define an initial state field to import forming

analysis results for the blank part instance

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d1 d1 Import element set BLANK from the

forming analysis

BLANK was the element set used for the blank section

definition in the original forming analysis

SHELL SECTION ELSET=BLANK

a requirement for input files not defined as

assemblies of part instances

In ABAQUSCAE and input files defined using parts

and assemblies part instances are specified for

import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1115

Import from ABAQUSExplicit to ABAQUSStandard

Keep blank and associated sets boundary conditions etc

ABAQUSCAE interface only

c1 Delete interactions rigid tools and associated sets

boundary conditions etc

c2

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1116

Import from ABAQUSExplicit to ABAQUSStandard

Define an initial state field to import forming

analysis results for the blank part instance

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d1 d1 Import element set BLANK from the

forming analysis

BLANK was the element set used for the blank section

definition in the original forming analysis

SHELL SECTION ELSET=BLANK

a requirement for input files not defined as

assemblies of part instances

In ABAQUSCAE and input files defined using parts

and assemblies part instances are specified for

import

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1117

Import from ABAQUSExplicit to ABAQUSStandard

Import the initial state field from

the end of the ABAQUSExplicit

forming analysis

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d2 d2 Import the blank from the end of the

ABAQUSExplicit forming analysis

If the STEP and INTERVAL

parameters are omitted

the data would be

imported from the last

available step and interval

for which restart data were

saved

Name of the forming

analysis job

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1118

Import from ABAQUSExplicit to ABAQUSStandard

Update the reference configuration

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YESBLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM

B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

d3 d3 Update the reference configuration

This option is used so that the reference configuration

is the deformed model prior to importing

The displacement field that ABAQUSStandard

calculates will be the amount of springback that

occurs

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1119

Import from ABAQUSExplicit to ABAQUSStandard

Define a boundary condition to

prevent rigid body motion of the

blank in the springback step

HEADING

Springback Calculation

IMPORT STEP=1 INTERVAL=1

UPDATE=YES

BLANK

STEPNLGEOM

STATIC

011

BOUNDARY

B1YSYMM B4XSYMM

BOUNDARY TYPE=VELOCITY

CORNER 3 3 00

END STEP

ABAQUSCAE interface Keywords interface

e e Define boundary conditions for the

springback step

B1

B4

CORNER

Respecify symmetry

boundary conditions

Imported node sets

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1120

bull The springback calculation is performed in ABAQUSStandard

ndash ABAQUSCAE interface job submission

ndash Keyword interface job submission

bull At the command prompt

abaqus job=DeepDrawBox_Springback oldjob=DeepDrawBox_Form

3

Import from ABAQUSExplicit to ABAQUSStandard

Name of ABAQUSStandard

springback analysis input fileName of ABAQUSExplicit

forming analysis job

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

7212019 l11 Interface

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

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Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1625

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1725

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 11: l11 Interface

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httpslidepdfcomreaderfulll11-interface 1125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1121

Import from ABAQUSExplicit to ABAQUSStandard

bull Equilibrium

ndash After importing the deformed blank and its current material state into

ABAQUSStandard the model will not be in static equilibrium

bull Two sets of forces contribute to this condition

ndash Dynamic forces

bull The forming process is simulated using a dynamic

procedure so inertia and damping forces are present

bull In a proper forming process simulation the state of dynamic

equilibrium is relatively close to a state of static equilibrium

ndash Boundary interaction forces

bull Changes in the boundary and contact conditions from the ABAQUSExplicit analysis to the ABAQUSStandard analysiscontribute to the lack of static equilibrium

bull Since springback involves the removal of contact conditions

this is the dominant contributing factor

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1122

Import from ABAQUSExplicit to ABAQUSStandard

ndash The initial out-of-balance forces are defined as those needed to achieve

static equilibrium

bull When the deformed blank is imported with the material state into

ABAQUSStandard a set of artificial internal stresses are applied that

equilibrate the imported stresses so that static equilibrium is obtainedat the start of the analysis

bull These artificial stresses are removed gradually during the springback

calculation step

bull As the stresses are removed the blank deforms further as a result of

redistribution of internal forces

bull The final (sprungback) configuration is achieved after complete

removal of the artificial stresses or initial out-of-balance forces

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1625

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1725

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 12: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1123

Import from ABAQUSExplicit to ABAQUSStandard

ndash The configuration of the

box forming analysis after

springback is shown in

the figure

deformed configuration after springback

contours of displacement magnitude

Deformed shape

scale factor = 10

as formed

after springback

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Import from ABAQUSStandard to

ABAQUSExplicit

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1625

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1725

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 13: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1125

Import from ABAQUSStandard to ABAQUSExplicit

bull Example Blade Containment

991251 983105 983139983151983149983138983145983150983137983156983145983151983150 983151983142 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140983137983150983140 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983145983155 983155983144983151983159983150 983156983151 983138983141983137983150 983141983142983142983141983139983156983145983158983141 983156983151983151983148 983142983151983154 983155983145983149983157983148983137983156983145983150983143 983137 983146983141983156983141983150983143983145983150983141 983138983148983137983140983141983085983151983157983156 983141983158983141983150983156983086

991251 983124983144983141 983142983137983150 983138983148983137983140983141 983137983155983155983141983149983138983148983161 983145983155 983145983150983145983156983145983137983148983148983161983155983156983137983156983145983151983150983137983154983161983086

991266 983127983141 983151983138983156983137983145983150 983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983151983142 983156983144983141 983141983150983143983145983150983141

983142983137983150 983138983148983137983140983141 983145983150 983105983106983105983121983125983123983087983123983156983137983150983140983137983154983140

991266 983124983144983141 983154983141983155983157983148983156983155 983151983142 983156983144983145983155 983137983150983137983148983161983155983145983155 983137983154983141983157983155983141983140 983137983155 983145983150983145983156983145983137983148 983139983151983150983140983145983156983145983151983150983155 983145983150 983156983144983141983140983161983150983137983149983145983139 983138983148983137983140983141 983154983141983148983141983137983155983141 983137983150983137983148983161983155983145983155983145983150 983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156983086

983105983106983105983121983125983123 983149983151983140983141983148 983151983142 983137983150 983137983145983154983139983154983137983142983156 983141983150983143983145983150983141983099

983138983148983137983140983141 983139983151983148983151983154983141983140 983154983141983140 983145983155 983154983141983148983141983137983155983141983140

bull The following example demonstrates the procedure for transferring

results from ABAQUSStandard to ABAQUSExplicit

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1126

Import from ABAQUSStandard to ABAQUSExplicit

bull Modeling approach

991251 983124983144983141 983154983141983155983157983148983156983155 983156983154983137983150983155983142983141983154 983139983137983152983137983138983145983148983145983156983161 983145983155 983157983155983141983140 983156983151 983156983154983137983150983155983142983141983154 983156983144983141 983155983156983137983156983141 983137983155983155983151983139983145983137983156983141983140 983159983145983156983144983156983144983141 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983155983151983148983157983156983145983151983150 983142983154983151983149 983156983144983141 983145983149983152983148983145983139983145983156 983155983156983137983156983145983139 983152983154983151983139983141983140983157983154983141 983156983151 983156983144983141983141983160983152983148983145983139983145983156 983140983161983150983137983149983145983139983155 983152983154983151983139983141983140983157983154983141983086

Import

ABAQUSStandard

Static procedure

Centrifugal Loading

Obtain associated stress state

fan only

ABAQUSExplicit

Import stress state

Initial Conditions Spin at appropriate velocity

Verify Steady state

Throw Blade

fan and

casing

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1625

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1725

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 14: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1127

bull The input syntax for ABAQUSStandard to ABAQUSExplicit import is

very similar to ABAQUSExplicit to ABAQUSStandard already discussed

ndash Request restart data during the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143983137983150983137983148983161983155983145983155983098

ndash The ABAQUSStandard analysis will produce the following files which will

be used to import the spinning fan into ABAQUSExplicit

bull Restart (res)

bull Analysis database (stt and mdl)

bull Part (prt) and

bull Output database (odb) files

Import from ABAQUSStandard to ABAQUSExplicit

RESTART WRITE FREQUENCY=100

The frequency options is only

available when requesting data for an

ABAQUSStandard analysis

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1128

Import from ABAQUSStandard to ABAQUSExplicit

ndash Import the ABAQUSStandard 983155983156983141983137983140983161 983155983156983137983156983141 983155983152983145983150983150983145983150983143 983154983141983155983157983148983156983155 983145983150983156983151 983156983144983141

983105983106983105983121983125983123983087983109983160983152983148983145983139983145983156 983138983148983137983140983141 983156983144983154983151983159 983149983151983140983141983148983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

The reference configuration will be

the original undeformed model

Import the fan

The sets HUB and BLADES

were used on the section

definition options for the

hub and the blades

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1625

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1725

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 15: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1129

Import from ABAQUSStandard to ABAQUSExplicit

ndash The engine casing which was not required in the ABAQUSStandard

steady state spinning analysis is defined in the ABAQUSExplicit blade

throw model983098

IMPORTSTEP=1 UPDATE=NO

HUB

BLADES

DEFINE CASING

NODE

10001 410 90 0

10002 410 300 0

10003 440 -100 0ELEMENT TYPE=S4RELSET=CASING

10001 1030510940109531030410002 10940109411095410953

10003 10941109421095510954

ABAQUSExplicit model

ABAQUSStandard model

casing

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1130

Import from ABAQUSStandard to ABAQUSExplicit

bull Loading

ndash In ABAQUSStandard we apply a centrifugal load about a defined axis

ndash In ABAQUSExplicit we apply an initial rotating velocity to the fan blades

bull Connector elements are used to attach a fan blade to the hub and

subsequently release the blade

DLOAD

3000 rpm --gt 314159 radsec --gt 98696044 (rads)^2

ROTOR CENTRIF 98696044 0 0 0 0 1 0

INITIAL CONDITIONS TYPE=ROTATING VELOCITY

ROTOR-N 314159 0 0 0

0 0 0 0 -1 0

centrifugal load

removed

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1625

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1725

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 16: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1625

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1131

bull Enhanced hourglass control

ndash Recommend for consistency between analyses

bull Second order accuracy element formulation

ndash The default first order element formulation in

ABAQUSExplicit is not appropriate for astructure subjected to several revolutions

Import from ABAQUSStandard to ABAQUSExplicit

bull Element section controls

ndash Element section controls are defined in the original analysis and cannot be

redefined in an import analysis

bull Material definitions can be redefined upon import

ndash In this example the following section controls are defined in the

ABAQUSStandard spinning analysis

SECTION CONTROLS NAME=ENHANCED

SECOND ORDER ACCURACY=YES

HOURGLASS=ENHANCED

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1132

Import from ABAQUSStandard to ABAQUSExplicit

ndash The enhanced hourglass control formulation is used so that hourglass

forces are consistently computed in both analyses

bull This leads to the reduction of noise in the import analysis solution

26E+07

28E+07

30E+07

32E+07

34E+07

36E+07

38E+07

40E+07

0 0002 0004 0006 0008 001

Analysis time (seconds)

I n t e r n a l e n e r g y

Version 63

Version 64Enhanced

Viscous

ABAQUSExplicit results for a steadily spinning disk (ie no blade release)

after importing results from ABAQUSStandard

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1725

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 17: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1725

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1133

Import from ABAQUSStandard to ABAQUSExplicit

bull Other modeling issues

ndash Use of general contact

bull The large number of potential interactions is readily handled with

general contact

ndash Use of double precision executable

bull Running in double precision is more suitable for this analysis because

of the high number of revolutions of the fan blade assembly

ndash Specifying a maximum stable time increment

bull By specifying a maximum time increment we guarantee that each

degree of revolution of the fan blade is analyzed over at least 10

increments

ndash We recommend a minimum of 10 analysis increments per degree

of revolution in problems involving finite rotations

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1134

Import from ABAQUSStandard to ABAQUSExplicit

bull Results

25 msec 5 msec

75 msec 10 msec

Many revolutions

(ie steady state verification)

Video Clip

Blade detachment

Video Clip

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 18: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1825

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Additional Import Modeling Issues

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1136

Additional Import Modeling Issues

bull Reference configuration

ndash For springback simulations the reference configuration is usually updated

bull The displacements strains step number and total time are reset to

zero for the current analysis

ndash For multi-stage forming simulations do not update the reference

configurationbull The displacements strains step number and total time are continued

from the previous analysis

Deformed shape

scale factor = 10

Reference configuration updated Reference configuration not updated

Reference

configuration

Reference

configuration

Deformed shape

scale factor = 1

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 19: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 1925

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1137

Additional Import Modeling Issues

bull Importing the material state

ndash By default the material state for each element is imported

bull This includes the stresses the orientation of the stresses and thefollowing state variables

ndash equivalent plastic strains and for Mises plasticity

ndash back stresses for the kinematic hardening models

ndash the maximum strain energy density during deformation history for

the Mullins effect

ndash user-defined state variables for user-defined constitutive models(user subroutines VUMAT and UMAT)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1138

Additional Import Modeling Issues

ndash If the material state is not needed set the

STATE parameter equal to NO on the

IMPORT option

bull All state variables are reset to zero

ndash ABAQUSCAE always imports thematerial state along with the deformed

mesh

bull If you want to import only thedeformed mesh you can import an

orphan mesh from a selected step

and increment of an output

database

IMPORT STATE = NO

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 20: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2025

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1139

Additional Import Modeling Issues

bull Reference configuration and material state

combinations

ndash UPDATE=NO STATE=YES

bull Continue the previous analysis (most

common usage)

ndash UPDATE=YES STATE=YES

bull Current stress applied to the current

configuration with no strain (similar to an

initial stress in a regular analysis)

ndash UPDATE=YES STATE=NO

bull Annealing ndash UPDATE=NO STATE=NO

bull (Awkward have strains but no stresses)

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1140

Additional Import Modeling Issues

bull Material definitions

ndash The material property definitions are imported by default

bull They can be redefined if necessary

bull If redefined

ndash The material names used for the imported elements must be the

same as the material names used in the previous analysis

ndash Caution should be exercised if changes are made to the material

properties

bull This may affect the initial out-of-balance forces

ndash The mass density may need to be redefined if mass scaling was

used in an ABAQUSExplicit simulation

bull If mass scaling is used the scaled masses will not be

transferred to the subsequent import analysis

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 21: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2125

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1141

Additional Import Modeling Issues

bull Element section definitions

ndash Element section property definitions are imported and may not be changed

from those used in the previous analysis

bull The current thickness of each shell element is imported automatically

bull Any material orientation information is imported automatically when

the material state is imported

bull Valid elements for importing

ndash The import capability is available for first-order continuum shell

membrane beam (both linear and quadratic) truss and rigid elements that

are common to both ABAQUSExplicit and ABAQUSStandard

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1142

Additional Import Modeling Issues

bull Geometric nonlinearity

ndash NLGEOM default settings

bull NO for ABAQUSStandard

bull YES for ABAQUSExplicit

ndash The setting of NLGEOM is imported and

becomes the setting in the newanalysis

bull The reference configuration cannot

be updated if NLGEOM=NO is

used because with small

deformation there is no reason to

update the configuration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 22: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2225

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1143

Additional Import Modeling Issues

bull Initial conditions and boundary conditions

ndash Valid initial conditions for various values of the STATE parameter are

shown below

bull New boundary conditions must be specified

ndash These may be different from those used in the previoussimulation

YES or NOVELOCITY

NOVOID RATIO

NOSTRESS

NOSOLUTION

YES or NOROTATING VELOCITY

NORELATIVE DENSITY

NOHARDENING

STATE=INITIAL CONDITIONS TYPE=

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Limitations

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 23: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2325

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1145

Limitations

ndash The same versions of ABAQUSExplicit and ABAQUSStandard must be

run on computers that are binary compatible

ndash The capability is not available for spring mass dashpot rotary inertia

connector fluid and infinite elements

ndash Contact definitions cannot be transferred

ndash Surface definitions (including analytical rigid surface definitions) cannot be

transferred

ndash Loads boundary conditions kinematic constraints (surface-based tie

coupling constraints etc) and nodal transformations are not imported

ndash Mesh-independent spot welds are not imported

bull However the spot weld reference nodes are imported and can beused to redefine spot welds in the import analysis

ndash In this case it is recommended that the reference configuration

be updated if large deformations occurred in the imported model

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1146

Limitations

ndash The complete material state (including state variables such as plastic

strains) is imported only for

bull linear elasticity

bull Mises plasticity (including the kinematic hardening models)

bull hyperfoam

bull hyperelasticity

bull Mullins effect

bull and the user materials (VUMAT and UMAT)

ndash Material stresses are imported for all valid material models

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 24: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2425

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1147

Limitations

ndash Analyses with predefined field variables andor temperature fields cannot

be imported

bull Temperatures are imported for coupled temperature-displacement and

adiabatic analyses if the material state is imported

bull Coupled temperature-displacement elements with predefined field

variable definitions can be imported however the field variable values

are not imported

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics

Demonstration

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis

Page 25: l11 Interface

7212019 l11 Interface

httpslidepdfcomreaderfulll11-interface 2525

Copyright 2005 ABAQUS Inc

ABAQUSExplicit Advanced Topics L1149

Demonstration

bull In this demonstration ABAQUSCAE is used to model the forming and

springback of an angled bracket

Play demo

with audioPlay demo

without audio

bracket_forming

The forming of half of a

symmetric angled bracket

is analyzed using

ABAQUSExplicit

Springback is analyzed in

ABAQUSStandard

An Initial state field is used to

import the final deformed

mesh and material state from

the ABAQUSExplicit forming

analysis