Page 268 - Mechanics of Asphalt Microstructure and Micromechanics
P. 268

260   Ch a p t e r  E i gh t


              are only the functions of local coordinate r, and are irrelevant to the other local coordi-
              nate, s. They can be written as:
                                                                       t+Δ t
                                                                         ⎡  •  ⎤
                                                                         ⎢ U 3 ⎥
                                                                           • ⎢  ⎥
                                                                         ⎢ V 3 ⎥
                                                                           • ⎢  ⎥
                                                                         ⎢   ⎥
                      t+Δ t                                              ⎢ U 4 ⎥
                         ⎧  •  ⎫                                         ⎢  •  ⎥
                         ⎪Δ W nt ⎪  ⎡ N  0  N  0   − N   0   − N    0 ⎤  ⎢ V 4 ⎥
                         ⎨    ⎬ = ⎢  3      4        1          2     ⎥          (8-53)
                         ⎪  •  ⎪  ⎣  0  N  3  0  N N 4  0  − N  1  0  − N 2 ⎦  ⎢  •  ⎥
                         ⎩ Δ W nn ⎭                                      ⎢ U 1 ⎥
                                                                           • ⎢  ⎥
                                                                         ⎢ V 1 ⎥
                                                                         ⎢  •  ⎥
                                                                         ⎢   ⎥
                                                                         ⎢ U 2 ⎥
                                                                         ⎢  • •  ⎥
                                                                            2
                                                                         ⎣ V ⎦
                     t+Δ t  ⎧ ⎫           t+Δ t  ⎡  •  •  •  •  •  •  •  •  ⎤
                         •
                 Let   ⎨ U ⎬  denote matrix   ⎢ U 3  V 3  U 4  V 4  U 1  V 1  U 2  V 2 , the corre-
                                                                           ⎥
                       ⎩ ⎭                  ⎣                              ⎦
              sponding strain rates would read:
                     t+Δ t
                        ⎧  •  ⎫  t+Δ t                                  t+Δ t  T
                        ⎪ε nt ⎪  1  ⎡ N  0  N   0  − N    0   − N   0 ⎤   ⎧ ⎫
                                                                            •
                        ⎨  ⎬ =    ⎢  3       4        1         2      ⎥  ⎨ U ⎬  (8-54)
                         •
                           ⎪
                        ⎪ ε nn ⎭  d  ⎣  0 0  N  3  0  N 4  0  − N 1  0  − N 2 ⎦  ⎩ ⎭
                        ⎩
                 On the upper and lower boundaries of the continuous interface element, local coor-
              dinate s is equal to 1 and –1, respectively. Hence,
                                         1−  r         1+  r
                                     N =     =  N ;  N =   =  N                  (8-55)
                                      1   2     4   2   2     3
                 The normal strain in the direction of the interface length is still taken as in a regular
              solid element. Therefore, total strain rates in continuous quadrilateral interface ele-
              ments are described as:
                  t+Δ t      t+Δ t
                     ⎧  •  ⎫   ⎡                                          ⎤
                     ⎪ ε nt ⎪  ⎢  N    0 0  N     0   − N    0   − N    0  ⎥
                        ⎪
                                                                                •
                     ⎪  • ⎪  ⎪  1  ⎢  3      4          1           2     ⎥  t+Δ t  ⎧ ⎫
                     ⎨ ε nn ⎬ =  ⎢  0  N  3  0   N 4   0   − N 1  0    − N ⎥  ⎨ U ⎬
                                                                                 ⎬
                                                                          2
                     ⎪  • ⎪  d  ⎢  ∂  s     ∂  s      ∂  s        ∂  s    ⎥   ⎩ ⎭
                     ⎪ε tt ⎪   ⎢ d  N  3  0  d  N  4  0  d d  N 1  0  d  N 2  0  ⎥
                     ⎩ ⎪  ⎭ ⎪  ⎣ ⎢  t ∂      t ∂        t ∂        t ∂    ⎦ ⎥
                                    + t Δ t ⎧ ⎫
                                       •
                             + t Δ
                          =  1  t  ⎡N  ' ⎤ ⎦  ⎨ ⎬
                                       U
                               ⎣
                           d          ⎩ ⎭
                                                                                 (8-56)
                         s
                                      s
                                s
                            s
                 Where  N ,  N ,  N and  N  are regular shape functions for a quadrilateral solid ele-
                         1  2   3     4
              ment.
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