CompoSIDE | Open · PDF fileCompoSIDE | Open Academy Webinar 2 ... Capabilities intro based on shell buckling example . Design of Shells ... CMDB LAMINASpace

CompoSIDE | Open Academy

Webinar 2 - Composite Shell Design 14/04/2015

Radek Michalik (Managing Director) & Aleksandra Dziekonska (Technical Support)

© 2014 CompoSIDE Ltd – All Rights Reserved

O b j e c t i ve s

2 © 2014 CompoSIDE Ltd – All Rights Reserved

Present CompoSIDE design capabilities

Show practical examples of shell structure design in CompoSIDE

14/04/2015

A ge n d a

14/04/2015 3 © 2014 CompoSIDE Ltd – All Rights Reserved

Why CompoSIDE ?

Introduction to FESpace

CompoSIDE Modules/Workflows

Practical Design Examples (Live Demo)

CompoSIDE Capabilities - Project Examples

Q&A

Why CompoSIDE?

© 2014 CompoSIDE Ltd – All Rights Reserved 14/04/2015 4

F ro m S ke t c h t o D e t a i l e d P ro d u c t D e s i g n …

14/04/2015 © 2014 CompoSIDE Ltd – All Rights Reserved 5

???

W hy C o m p o S I D E ?


6

W hy C o m p o S I D E #1


Collaboration &

Integration

W hy C o m p o S I D E ? #2


Composites Focused



Centralized Data Management



Agile Workflows



Automated Documentation



Flexible Licensing

Introduction to FESpace


LAMINASpace

FESpace

BOMGen

REPORTSpace CMDB

F E S p a c e I n t ro d u c t i o n


FESpace interface

Capabilities intro based on shell buckling example

D e s i g n o f S h e l l s - B u c k l i n g C h e c k


Curved Shell buckling check & iteration

Shell Geometry

Parameters Units Value

Length [mm] 3000

Radius [mm] 2000

Width [mm] 800

Buckling Results Summary

What happened?

F E S p a c e - Re s u l t s

Date: 14/04/2015 © 2014 CompoSIDE Ltd – All Rights Reserved Slide: 16

Model BLF

Critical Strains

[%]

Critical Load

[N/mm] Critical

Load [kN] Weight

[Kg]

Model 1 – (Baseline) 0.38 0.125% 3057.5 2246 80.68

Model 2 – (Base+Tapes) 0.40 0.132% 3781.6 2800 86.54

Buckling Load Factor BLF

Shell Thickness t [mm]

Base (Model 1) 0.38 19.66

Base+ Tapes (model 2) 0.40 22.84

BLF2/BLF1 1.053

(t2/t1)^1/3 1.051

CompoSIDE Modules/Workflows


C o m p o S I D E M o d u l e s / Wo r k f l o ws


PROJECTSpace

CMDB

LAMINASpace

FESpace

BOMGen

REPORTSpace

Downstream Design

Upstream Modifications

Live Design Demo


Composites Plate Design

D e s i g n B r i e f – F l a t Pa n e l D e s i g n ( 1 )


Design composite plate to meet the design criteria:

Parameters Units Value

LOADS /SF

Working Pressure [MPa] 0.05

Ultimate Load Partial Safety Factor [-] 2.7

Boundary Conditions / Edge Support All edges simply

Supported

Plate Geometry

Length [mm] 3000

Width [mm] 900

Max Thickness [mm] 40 Design Targets

Max. Weight [kg] 25

Max. Material Cost [€/m^2] 250

Max. Working Deflection [mm] 10

Min. Natural Frequency above [Hz] 100

P R OJ E C T S p a c e / C M D B


PROJECTSpace

CMDB

LAMINASpace

FESpace

BOMGen

REPORTSpace

M a t e r i a l S e l e c t i o n


L A M I N A S p a c e


PROJECTSpace

CMDB

LAMINASpace

FESpace

BOMGen

REPORTSpace

P re l i m i n a r y D e s i g n i n L A M I N A S p a c e


Max. Working Loads (1st Principle)

Shear Force (Qy) 22 [N/mm]

Bending Moment (My) 5060 [Nmm/mm]

Sandwich Laminate

¤ Pre-preg/PVC foam

Strip Beam approximation

¤ Working Loads:

Verification:

¤ Strength (Ultimate Load)

• Fibre Failure /Core Shear

¤ Local Stability (Wrinkling)

Qy

Qy

Mymax

F E S p a c e


CMDB

PROJECTSpace

LAMINASpace

FESpace

BOMGen

REPORTSpace

F E M o d e l C re a t i o n - P l a t e


B O M G e n


PROJECTSpace

CMDB

LAMINASpace

FESpace

BOMGen

REPORTSpace

B i l l o f M a t e r i a l G e n e ra t i o n


R E P O R T S p a c e


PROJECTSpace

CMDB

LAMINASpace

FESpace

BOMGen

REPORTSpace

B o M Re p o r t G e n e ra t i o n


D e s i g n S u m m a r y


CMDB

PROJECTSpace

LAMINASpace

FESpace

BOMGen

REPORTSpace

Panel Design Results

F E S p a c e – Re s u l t s S u m m a r y


Fibre Failure RF Core Failure RF

D e s i g n C o st Tra n s p a re n c y


Flat Panel Design CU Summary CU

LAMINASpace - Included in Subscription

FESpace - Static Run 16 2 iterations & 2 load cases

FESpace - Failure 3 1 iterations & 1 load case

BOM Creation 25 One off (updates free)

Laminates Table Export for CAD 6 For one component

BoM Report Generation 25

Total CompoSIDE Units (CU) 75

Approximate Cost (€) € 7.5 CU’s cost: € 0.1 (CU-8000 Plan)

G e t s t a r t e d !


Sign up for 30 days free trial!!

¤ CU-1000 Recommended for low monthly use of FESpace

¤ CU-8000 Recommended for heavy FESpace Users

Project Examples


Shell Design Examples

C o m p o s i t e B r i d ge – S h e l l D e s i g n

36 © 2014 CompoSIDE Ltd – All Rights Reserved 14/04/2015

Bridge Geometry and Load Case Visualization

Bridge Deformation

C o m p o s i t e B r i d ge


Internal Forces (In-Plane)

Modal Analysis – 1st Mode

P re s s u re Ve s s e l D e s i g n


Geometry (1/8th)

Boundary Conditions and Loading

P re s s u re Ve s s e l D e s i g n


Total Deformation

O t h e r S h e l l D e s i g n E xa m p l e s


Extruded Airfoil – Wing Panel

L-Flange Beam - Twisting

Shells with Cut-outs and beam elements

Questions & Answers


S u p p o r t & Tra i n i n g


Support

FAQs

CompoSIDE Tutorials

Webinars

Knowledge Base

www.composide.com/support-and-training

N e e d H e l p ?


Email: [email protected]

Support & Knowledge Base Portal

Support Chat

Technical Documentation TechDocs

YouTube Channel Tutorials

mailto:[email protected]

G e t s t a r t e d !


Sign up for 30 days free trial!!

Thank you


Documents

CompoSIDE | Open · PDF fileCompoSIDE | Open Academy Webinar 2 ... Capabilities intro based on shell buckling example . Design of Shells ... CMDB LAMINASpace