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Two-Dimensional Elasticity                                                  119



                         (a)                          (b)
                                       z

                                                                             y
                                           y
                                  x

                                                                   x

            FIGURE 4.3
            Plane stress condition: (a) structure with in-plane loading; and (b) 2-D model.


                         (a)                            (b)
                                    y                           y
                                      x
                                      z                                 x








            FIGURE 4.4
            Plane strain condition: (a) structure with uniform transverse load; and (b) 2-D model.


            4.2.3  Stress–Strain (Constitutive) Equations
            For linear elastic isotropic materials, we have the following strain–stress relation for the
            plane stress case:

                                 ε    1/ E  −ν E/   0   σ x     ε x0  
                                                          
                                   x
                                                          
                                                               
                                          /
                                  ε  = −ν E   1/ E   0    σ y  +   ε y0         (4.3)
                                       
                                   y
                                      0       0    1/ G         
                                                          τ xy
                                 γ xy                        γ xy0 
            or,
                                             ε= E −1
                                                    σ+ ε 0
            where ε  is the initial strain (e.g., due to a temperature change), E Young’s modulus, ν
                   0
            Poisson’s ratio, and G the shear modulus. Note that

                                                     E
                                              G =                                      (4.4)
                                                  21 (  + )ν

            for homogeneous and isotropic materials.
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