269
Solutions Manual Elasticity: Theory, Applications and Numerics Second Edition By Martin H. Sadd Professor Department of Mechanical Engineering & Applied Mechanics University of Rhode Island Kingston, Rhode Island Foreword Exercises found at the end of each chapter are an important ingredient of the text as they provide homework for student engagement, problems for examinations, and can be used in class to illustrate other features of the subject matter. This solutions manual is intended to aid the instructors in their own particular use of the exercises. Review of the solutions should help determine which problems would best serve the goals of homework, exams or be used in class. The author is committed to continual improvement of engineering education and welcomes feedback from users of the text and solutions manual. Please feel free to send comments concerning suggested improvements or corrections to [email protected] . Such feedback will be shared with the text user community via the publisher’s web site. Martin H. Sadd January 2009 Copyright © 2009, Elsevier Inc. All rights reserved.

Sadd Elasticity Solutions Manual

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  • Solutions Manual

    Elasticity: Theory, Applications and Numerics Second Edition

    By

    Martin H. Sadd

    Professor Department of Mechanical Engineering & Applied Mechanics

    University of Rhode Island Kingston, Rhode Island

    Foreword

    Exercises found at the end of each chapter are an important ingredient of the text as they provide homework for student engagement, problems for examinations, and can be used in class to illustrate other features of the subject matter. This solutions manual is intended to aid the instructors in their own particular use of the exercises. Review of the solutions should help determine which problems would best serve the goals of homework, exams or be used in class. The author is committed to continual improvement of engineering education and welcomes feedback from users of the text and solutions manual. Please feel free to send comments concerning suggested improvements or corrections to [email protected]. Such feedback will be shared with the text user community via the publishers web site. Martin H. Sadd January 2009

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-1.

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    Copyright 2009, Elsevier Inc. All rights reserved.

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    Copyright 2009, Elsevier Inc. All rights reserved.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-5.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-7.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-12.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-12.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-12.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-14.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-15.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-17.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-18.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 1-18. Continued

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    Copyright 2009, Elsevier Inc. All rights reserved.

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  • 2-1.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-2.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-3.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-4.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-5.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-6.

    ++++++

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-8*.

    bygiven isPlot MATLAB The

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-9*.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-10*. MATLAB CODE % Principal Value Problem % Enter strain matrix e=[2,-2,0;-2,-4,1;0,1,6]*0.001; % Calculate principal values L and directions N [N,L]=eig(e); fprintf('Principal Values') disp(diag(L)') fprintf('Principal Directions') N1=N(:,1)' N2=N(:,2)' N3=N(:,3)' SCREEN OUTPUT >> Principal Values -0.0047 0.0026 0.0061 Principal Directions N1 = -0.2852 -0.9543 0.0893 N2 = 0.9570 -0.2784 0.0815 N3 = -0.0529 0.1087 0.9927 2-11.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-13.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-15.

    ( ) ( )( )

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-17.

    00)2.6.2(3246)22(2662(2.6.2)

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-19.

    +

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 2-20.

    ( ) ( )( )

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 0 0.5 1 1.5 2 2.5 3 3.53.5

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-3.

    +=++==

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-4.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-6.

    ( )

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    Copyright 2009, Elsevier Inc. All rights reserved.

    www.mechanicspa.mihanblog.com

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  • 3-8*. Using MATLAB the first principal stress contours are:

    3-9.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-10*.

    : Plotand Code MATLAB

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    % Exercise 3-6 % Maximum Shear Stress Contours for Flamant Problem clear; % Generation of variable space [x,y]=meshgrid(-3:0.05:3,0:0.05:3); % Calculation of Nondimensional Maximum Shear Stress sxy=y./(x.^2+y.^2); hold on axis equal axis off % Plot contours with reversed y-axis contour(x,-y,sxy,20);

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-12.

    21

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-14.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-17.

    3/632

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-19.

    yxxy

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    3-20.

    satisfiedy identicall are equations mequilibriuboth

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    Copyright 2009, Elsevier Inc. All rights reserved.

    www.spowpowerplant.blogfa.com

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  • 3-21.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-22.

    equations. mequilibriu esatisfy thnot do stresses materials of mechanics eapproximat The

    000

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 3-25.

    ( )

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    0)(11 gives forcebody edappropriat the

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    1

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 4-1.

    =

    +++++=+++++=+++++=+++++=+++++=+++++=

    +++++=+++++=+++++=+++++=+++++=+++++=

    313131233112313331223111

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 4-3.

    ijijkkij

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    +==+=

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    ++++=

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 4-7.

    kkiieii

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    2 and imply that then materials isotropicfor results These

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 4-9.

    plane in the beamr rectangula a of bending pure toscorrespond stress of state thisThus0 2

    0 2)(

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 4-12.

    3-

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 4-13.

    ijijkkijijkkijijkkij

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    4-15.

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    [ ] [ ][ ] [ ][ ] [ ]

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 4-17.

    [ ][ ][ ] TT

    Ee

    TTTETE

    e

    TETE

    e

    e

    yxzz

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    +=+=+==

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    equation original thefrom follow stressesShear

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-1.

    p 40o

    x

    y

    a

    b

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    x

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    ======

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-1. Continued

    5-2.

    p

    a b

    r

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    TTTTTTTTTT

    nnTnnTnn

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-3.

    0),(,2),(

    0),(,02),(

    0),0(,02),0(

    0)0,()0,((a)

    =

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    0)cos(2sin

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-4. Continued

    ),(),(,),(),(

    ),(),(,),(),(:Conditions Interface

    0),(,),(:(2) Material

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    ====

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-6.

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-9.

    021

    1

    01)21(

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    )1(2)21)(1(

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-10.

    ])([2

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-11.

    theory.SOMth exactly wimatch results elasticity the,2

    ,2

    , constantsWith

    )(2

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 5-12.

    solution. elasticityproper a not are thusand ity,compatibilnot but mequilibriusatisfy stresses

    check)not (does0)1(40)])(1([)]([)1(

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • x

    y / P

    xy / P

    y = 10a

    x

    y / P

    xy / P

    y = 100a

    5-13*.

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    +=+=+=

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 6-1.

    xxxx

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 6-4.

    ( ) ( )mnmnmnkkmnmnkkmnjj

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 6-7.

    ( ) ( )221212212

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 6-11.

    )1(821

    211

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 6-13.

    EIlq

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    ,

    ====

    ====

    ====

    ===

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-1.

    xyxyxyxyxy

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    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-2.

    +

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    xyxyxyyyxx

    y

    x

    yyyxy

    xxxyx

    xyyx

    )()1(

    givesrelation ity compatibil intoresult thisusing and,2

    0

    0

    equations, mequilibriu fromBut

    2)()1(

    12])1[(1])1[(1

    2

    1,])1[(1,])1[(1:Equationity Compatibil Michell-Beltrami

    0)()

    0)()

    02)()(0

    0)(2)(0

    )(,2)(,2)(

    :Equations sNavier'

    2

    2

    2

    2

    22

    2

    2

    2

    2

    2

    2

    2

    2

    2

    222

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    2

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-3.

    00(b)(a)

    00(a)(b)

    (b)

    0)()(

    (a)

    0)()(

    0)(,0)(:equationsNavier

    4

    4

    22

    22

    22

    22

    22

    ==

    ==

    +

    =

    =

    +

    +

    ++

    +

    +

    +

    ++

    =

    =

    +

    +

    ++

    +

    +

    ++

    =+

    +

    ++=+

    +

    ++

    vyx

    uyx

    vy

    ux

    Fyv

    xu

    yv

    yF

    yv

    xu

    xu

    x

    vx

    uy

    Fyv

    xu

    yv

    xF

    yv

    xu

    xu

    y

    Fyv

    xu

    yvF

    yv

    xu

    xu

    yx

    yx

    yx

    7-4.

    =

    ==++==+==

    =

    ==++==+==

    ==++=

    =+==

    ++=+=+=

    A zy

    AyyAA z

    A

    czzA

    Tzy

    A zx

    AxxAA z

    A

    czzA

    Tzx

    A zAA z

    A

    czzA

    Tzz

    czyxz

    czz

    Tz

    xdAI

    A

    dAxIAIdACxBxyAxxdA

    xdAxdAM

    ydAI

    B

    dAyIBIdACyByAxyydA

    ydAydAM

    dAA

    CACdACByAxdA

    dAdAR

    A

    CByAx

    2

    2

    )(

    )(

    2

    2

    )(

    )(

    )(

    )(

    )(

    )()(

    1

    where,axes) principal(for )(

    0)(0

    1

    where,axes) principal(for )(

    0)(0

    :endsat momentsresultant zeroFor 1axes) principal(for )(

    0)(0

    :section -cross with endsat forceresultant zeroFor

    ,)(

    sum, assolution totalChoose

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-5.

    ( )( )

    checks alsowhich ,)1( )()(

    )(satisfy alsomust stress normal plane-of-out The

    000)(1

    1)(

    000210

    000210

    :equationsity compatibil and equilbriumsatisfy must Stresses

    22

    2

    2

    ykxkxkxy

    kxkxyyF

    xF

    kxy

    kyx

    Fyx

    kyy

    kxyx

    Fyx

    yx

    yxz

    yxyx

    yyxy

    xxyx

    +=+=++=

    ==+

    +

    =+

    ==+

    =++

    ==

    +=+

    +

    7-6.

    xyxyxyxy

    xyyyxyxy

    yxxyxyxx

    yxyx

    yxyx

    xyy

    yxx

    eEE

    e

    eeEeeEeeE

    eeEeeEeeE

    eeE

    eeE

    Ee

    Ee

    +=+=

    +=++=

    +=+++=

    +=+=+

    ==

    11

    )(1

    )(1

    )(1

    2

    )(1

    )(1

    )(1

    2

    )(1

    )(1

    )(1

    )(1

    2

    2

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-7.

    +

    +=+

    +

    =+

    +

    +

    ==+

    +

    +

    ==+

    +

    +

    +=++

    +=

    +

    =+

    +===

    =+

    +

    +

    =+

    +

    +

    +

    +

    =+

    +

    +

    +

    +

    =++

    =+

    +

    +

    =+

    +

    ++

    +

    =+

    +

    +

    +

    +

    =++

    +

    +=

    +

    =

    +

    =

    yF

    xF

    yF

    xF

    yxyx

    xyyyF

    Fyx

    yxxxFF

    yx

    yxyx

    EyxExEyyxe

    xe

    ye

    Ee

    Ee

    Ee

    Fyv

    xu

    yEv

    Fxy

    uyvE

    xv

    yxuE

    Fxu

    yvE

    yxv

    yuE

    xF

    yx

    Fyv

    xu

    xEu

    Fxyv

    yuE

    yxv

    xuE

    Fxv

    yuE

    yyv

    xuE

    xF

    yx

    xv

    yuE

    xu

    yvE

    yv

    xuE

    yxyx

    yxyxxy

    xyyyy

    yxy

    xyxxx

    xyx

    yxxyyx

    xyxyyxxyyx

    xyxyxyyyxx

    y

    y

    yyyxy

    x

    x

    xxxyx

    xyyx

    )1()(

    givesrelation ity compatibil intoresult thisusing and,2

    0

    0

    equations, mequilibriu fromBut

    2)()1(

    1

    12)(1)(12

    1,)(1,)(1:Equationity Compatibil Michell-Beltrami

    0)1(2

    01)1(2

    01)1(2

    0

    0)1(2

    0)1(21

    0)1(21

    0

    :equations mequilibriu into Substitute)1(2

    ,1

    ,1

    2

    2

    2

    2

    22

    2

    2

    2

    2

    2

    2

    2

    2

    2

    222

    2

    2

    2

    2

    22

    2

    2

    2

    2

    2

    2

    2

    2

    22

    22

    2

    2

    2

    2

    22

    2

    2

    2

    2

    22

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-8.

    l.dimensiona- threebe willfield the thusand , coordinateplane-of-out on the depend willntsdisplaceme theimply that results These

    functionsarbitrary are and where

    ),(210

    21

    ),(210

    21

    , offunction )(1

    that Note

    functionarbitrary an is ),( where,),(

    2

    2

    z

    hg

    yxhzxfz

    xev

    xfz

    xe

    zu

    xw

    zue

    yxgzyfz

    yev

    yfz

    ye

    zv

    yw

    zve

    yxeee

    yxfyxfzewzwe

    zzxz

    zzyz

    yxz

    zz

    +

    =

    ==

    +

    =

    +

    =

    ==

    +

    =

    =+=

    +==

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-9.

    problem. general afor satisfied benot willrelationsity compatibil thegintegratin fromresult theso and linear, benot willfieldstrain or stress plane-in thegeneralIn

    )(1

    )((7.2.2)Relation

    constantarbitrary an is where,)()()(

    )()(

    )( and constant)(0)()(0

    )(0

    )(0

    :gives results three thesengIntergrati

    0

    02

    02

    :aren formulatio stress plane in the includednot e which werrelationsity compatibil vanishing-non threeThe

    3

    2

    2

    2

    2

    2

    22

    2

    22

    2

    2

    2

    2

    2

    22

    2

    2

    2

    2

    yxyxz

    z

    z

    zz

    z

    zz

    zz

    zzxyzxyz

    zzxxz

    zyzzy

    eeE

    e

    cbyaxe

    ccbyyFbyFbxgye

    yFaxeayfxe

    bxgayfxgyfyx

    e

    xgye

    ye

    yfxe

    xe

    yxe

    ye

    xe

    ze

    zyxe

    xe

    xze

    ze

    xe

    ye

    zye

    ye

    ze

    +=+=

    ++=+====

    +===

    ======

    =

    =

    ==

    =

    +

    +

    =

    =

    =+

    =

    =

    +

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-10.

    case!either for changenot does modulusshear that theNotice

    )1(2)1(21

    )1()21(

    )1

    1(2

    )1()21(

    )1(2

    )1)(1()21)(1()1(

    )1()21(

    )1

    21)(1

    1(

    1)1()21(

    )21)(1(

    :stress plane strain to Plane

    )1(2)1(21

    1)1

    1(2

    1)1(2

    )31)(1()21)(1()1(

    1)1

    21)(1

    1(

    11)21)(1(

    :strain plane tostress Plane

    2

    2

    2

    2

    2

    2

    2

    2

    =+=+++

    ++=

    ++++

    =+=

    +=+++

    +++=

    ++

    ++

    ++

    =+=

    =+=+

    =

    +=+=

    +=+

    =

    +

    =+

    =

    EEE

    E

    EEE

    E

    EEE

    E

    EEE

    E

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-11.

    +

    =+

    +

    +=+

    +

    +=+

    =+

    +

    ++

    =+

    +

    ++=+

    +

    +

    =+

    +

    +

    +

    +=+

    +

    +

    =+

    +

    =+

    =+

    +

    +

    =+

    +

    ++++

    =+

    +

    ++

    yF

    xF

    yF

    xF

    yF

    xF

    Fyv

    xu

    xu

    Fyv

    xu

    xEuF

    yv

    xu

    x

    E

    u

    Fyv

    xu

    xEu

    yF

    xF

    yF

    xF

    yF

    xF

    Fyv

    xu

    xEu

    Fyv

    xu

    xEEu

    Fyv

    xu

    xu

    yxyx

    yxyx

    yxyx

    x

    xx

    x

    yxyx

    yxyx

    yxyx

    x

    x

    x

    11)()

    11()(

    )1()( : (7.2.7)Equation

    (7.2.5)relation for Likewise

    0)(: toreduceswhich

    0))1)(1(2

    0))

    11(2

    1

    1-7 Table from results theusingstrain plane toConverting

    0))1(2

    :(7.2.5)Equation (b)

    )1()(

    11

    1)(

    11)(: (7.1.7)Equation

    (7.1.5)relation for Likewise

    0))1(2

    : toreduceswhich

    0))1(2)1)(1(

    (

    10-7 Exercise from results theusing stress plane toConverting

    0)(:(7.1.5)Equation (a)

    22

    2

    2

    2

    22

    2

    21

    22

    2

    2

    2

    2

    21

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-12.

    1.-7 Exercisein given sexpression match withproperly Results

    1

    1

    111

    ])1[(11

    1)(1

    ])1[(11

    1)(1)31)(1(

    ,,1

    ,1

    :Strain Plane Stress Plane (b)

    6.-7 Exercisein given sexpression match withproperly Results1

    22

    )(11

    )()1)(1(

    2)( :Likewise

    )(11

    )()1)(1(

    2)(

    )1)(1(,,

    1,

    )1()21( :Stress Plane Strain Plane (a)

    2

    2

    2

    2

    2

    2

    2

    xyxyxyxy

    xyxyxyy

    yxyxyxx

    xyxyxyxy

    xyyyxyyxy

    yxxyxxyxx

    EEEe

    EEEe

    EEEe

    EEE

    Eee

    eeEeEeeEeee

    eeEeEeeEeee

    EEE

    +=

    +

    +=

    +=

    =

    +=

    =

    +

    +==

    +=++++++=

    +=++++++=

    ++

    ++

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-13*.

    bygiven are ntsdisplacemestrain plane and stress plane theof plots MATLAB, Usingidentical. become ntsdisplaceme two the0, ratio sPoisson'When

    12

    )1(/

    ][2

    )1(

    121

    /][

    2

    :0) ( aixs- Along12

    )1(,)1( :ResultsStrain Plane

    1,

    1 :Strain Plane Stress Plane

    ,][2

    , :Results Stress Plane

    22

    2.22

    2

    .

    2

    2.22

    .

    2222

    2

    2

    222

    ==

    ==

    =

    +==

    +==

    lx

    EIMlvlx

    EIMv

    lx

    EIMlvlx

    EIMv

    yx

    lxyEI

    MvEI

    Mxyu

    EE

    lxllxyEIMv

    EIMxyu

    StrainPStrainP

    StressPStressP

    -1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.8 1

    -0.5

    -0.4

    -0.3

    -0.2

    -0.1

    0

    Dimensionless Distance, x/l

    Dim

    ensi

    onle

    ss D

    ispl

    acem

    ent,

    v(x,

    0)/(M

    l 2/E

    I)

    Exercise 7-13 Note |v-plane stess| > |v-plane strain|

    plane stessplane strain

    n=0.4

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-14*.

    bygiven are ntsdisplacemestrain plane and stress plane theof plots MATLAB, Usingidentical. become ntsdisplaceme two the0, ratio sPoisson'When

    /1

    11)1(

    /)(

    ,/1)21()1(

    /)(

    :lizingdimensiona-Non

    111

    121

    )1()21(

    )1

    1(

    1,

    )1()21( :Stress Plane Strain Plane

    )21()1( :ResultStrain Plane

    111

    .

    111

    .

    21

    21

    2

    2

    21

    +++=

    ++=

    +++=

    +

    +

    +++

    +=

    ++

    +

    ++=

    rrrr

    ETru

    rrrr

    ETru

    rrr

    ET

    rrr

    E

    Tu

    EE

    rrr

    ETu

    StressPrStrainPr

    r

    r

    0 1 2 3 4 5 6 7 8 9 100

    2

    4

    6

    8

    10

    12

    14

    16

    18

    20

    Dimensionless Distance, r/r1

    Dim

    ensi

    onle

    ss D

    ispl

    acem

    ent,

    u r /(

    Tr1

    /E)

    Exercise 7-14 Note |ur-plane stess| > |ur-plane strain|

    plane stessplane strain

    n=0.4

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.50

    0.5

    1

    1.5

    2

    2.5

    Poisson Ratio,

    Dim

    ensi

    onle

    ss B

    ound

    ary

    Dis

    plac

    emen

    t, u r

    /(Tr

    1 /E

    )Exercise 7-14 Note |ur-plane stess| > |ur-plane strain|

    plane stessplane strain

    7-15.

    VyV

    xVV

    xV

    y

    yF

    xF

    VyV

    xVV

    xV

    y

    yF

    xF

    yVF

    xVF

    yxV

    xV

    y

    yxyx

    yxyx

    yxxyyx

    242

    2

    2

    2

    2

    2

    2

    22

    2

    242

    2

    2

    2

    2

    2

    2

    22

    2

    2

    2

    2

    2

    2

    )1()1()(

    )1()(:Stress Plane

    121

    11)(

    11)(:Strain Plane

    ,,,,

    =

    +

    +=+++

    +

    +=+

    =

    +

    =+

    ++

    +

    =+

    =

    ==+

    =+=

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-16.

    +

    =++=

    +=+=

    =

    +

    ++

    +

    +

    +

    ++

    ++

    +

    =++=

    =

    =

    ==

    ==

    ++

    ++

    +=

    +

    +=

    +

    =

    +

    ++

    =+=

    =

    +

    ==

    =

    ru

    ruu

    reeee

    urr

    ueeee

    ru

    xu

    xu

    xu

    xu

    yu

    yu

    yu

    yu

    yu

    yu

    yu

    yu

    xu

    xu

    xu

    xu

    eeeerryrrx

    ryxryrx

    xu

    xu

    xu

    xu

    yu

    yu

    yu

    yu

    uux

    uuyx

    vyue

    yu

    yu

    yu

    yuuu

    yyve

    xu

    xu

    xu

    xuuu

    xxue

    rxyyxr

    rxyyx

    r

    rr

    rr

    rr

    rr

    xyyxr

    rr

    rr

    rrxy

    rr

    ry

    rr

    rx

    121)sin(coscossincossin

    1cossin2cossin

    , Likewise

    cossincoscossinsin

    sinsincoscos

    sincoscossinsin

    cossinsincoscos

    cossin2sincos

    cossin,sincos

    cossincossin,cossin,sincos

    coscossinsinsinsincoscos21

    )cossin()sincos(21

    21

    coscossinsin)cossin(

    sinsincoscos)sincos(

    22

    22

    2

    2

    22

    22

    Copyright 2009, Elsevier Inc. All rights reserved.

  • 7-17.

    02

    2

    11

    2

    121,1,

    :Relationsnt Displaceme-Strain

    2

    22

    2

    2

    2

    2

    2

    3

    2

    22

    2

    2

    222

    2

    2

    2

    =

    +

    =

    =

    +

    =

    +

    +=

    +

    +

    +=

    +=

    +

    =

    +==

    rrr

    rrrrrr

    rr

    rr

    rr

    rr

    rrr

    rr

    erer

    rerer

    r

    rere

    rur

    ru

    ruruu

    rrerer

    r

    ru

    ruruu

    ru

    ru

    ruu

    rr

    r