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F inite Element Method and Boundar y Element Method   247


                               ⎡ N 00,,, N 00,, ... N 00,, ⎤
                               ⎢  1     2      r   ⎥
                               ⎢
                           N = 0,  N 0 0, , , N 0 0, ... , N ,0 ⎥
                                                r r
                                         2
                                   1
                               ⎢ 00  N ,,,  N ... ,, N  ⎥
                                      00
                                 ,,
                                             00
                               ⎣     1     2      r ⎦
                           u =  Nu q                                             (8-26)

                 Step 3: Formulation of Element Properties
                 The objective of this step is to conduct element-level integration to associate node
              displacements with equivalent node forces. There are three typical approaches: the di-
              rect approach, the variational approach, and the weighted residual approach. The ma-
              jor technique is to represent the volume integration (energy, forces) of the element in
              terms of node variables.
                 Equation (8-1) can be represented in the following format:
                           ε = Lu                                                (8-27)
                           ε = ( ε , ε , ε ,2 ε ,2 ε ,2 ε ) T
                               11  22  33  12  23  13
                              ⎡  ∂     ⎤
                              ⎢  ,,    ⎥
                                  00
                              ⎢ x 1    ⎥
                              ⎢   ∂    ⎥
                              ⎢ 0,  0 ,  ⎥
                              ⎢   x ∂  2  ⎥
                              ⎢    ∂   ⎥
                              ⎢ 00 ,,  ⎥
                           L =  ⎢ ⎢  x ∂  3  ⎥ ⎥ ⎥
                              ⎢  ∂  ∂  ⎥
                              ⎢  x ∂  ,  x ∂  0 ,  ⎥
                              ⎢  2   1  ⎥
                              ⎢   ∂  ∂ ∂ ⎥
                              ⎢ 0,  x ∂  ,  x  ⎥
                              ⎢    3  2  ⎥
                              ⎢  ∂   ∂ ⎥
                              ⎢ ∂x  0 ,,  ∂x  ⎥
                              ⎣  3    1  ⎦
                 Please note the difference between Cauchy strain and the engineering strain for the
              shear components. The corresponding coefficients for Hooke’s law should be adjusted
              by a factor of one-half.
                           q
                 Since u = Nu , e = Lu.
                 Denote B = LN, one has:
                                               ε = Bu q                          (8-28)
                 Denote the matrix format of the elasticity tensor as C (6   6 matrix); one has the fol-
                                                                            T
              lowing stress-strain relation (in vector format,  σ = ( σ , σ , σ , σ , σ , σ ) ):
                                                                33
                                                                   12
                                                                       23
                                                             22
                                                                          13
                                                          11
                                               σ = C ε                           (8-29)
                 The total strain energy in Equation (8-23) can be considered as the sum of the strain
              energies of the elements.
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