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F inite Element Method and Boundar y Element Method   259


                 Where Δ denotes the difference between the upper and lower surface quantities,
                                          •    •
              • denotes the rate of quantities, U and V are the tangential and normal displacement
                                               •       •
              rates under coordinate system t-o′-n, ΔW t  and ΔW n  are the relative tangential and nor-
                                                C
                                                         C
              mal displacement rates, respectively.  t+Δt N A  and  t+Δt N B  are given by:
                                     t+Δ t N =−  t+Δ t r  t+Δ t N =  t+Δ t r     (8-49)
                                         C
                                                        C
                                            1
                                         A       c      B     c
                 In which  t+Δt r c is simply obtained as the ratio of the length of segment AC to the
              length of segment AB. Here, point C is the image of point K on boundary AB. The loca-
              tion of point C is determined by assuming that KC and AB in Figure 8.3(a) are inter-
              sected at a right angle. As a result, the corresponding strain rates in the element as de-
              scribed in Section 2 take the form:
                                     t+Δ t
                                       ⎧  •  ⎫           t+Δt
                                                          Δ
                                       ⎪ε nt ⎪  1  t+Δ t    ⎧ ⎫
                                                             •
                                       ⎨ •  ⎬ =  t+Δ t  ⎡N  int ⎤ ⎦  ⎨ U ⎬
                                                    ⎣
                                       ⎪ ε nn ⎭ ⎪  d        ⎩ ⎭
                                       ⎩                                         (8-50)
                 Where thickness   t+Δt d of the interface element, written as d hereafter, is calculated
              from current coordinates of points K and C, and will be updated continuously. As men-
              tioned before, the normal strain parallel to the interface is taken as:
                               t+Δ t  •  ⎡ ∂ N  ∂ N    ∂ N   ⎤  t+Δ t ⎧ ⎫
                                                                  •
                                  ε tt =  ⎢  t ∂  A  0  t ∂  B  0  t ∂  K  0 ⎥  ⎨ U ⎬
                                                                   ⎬
                                      ⎣                      ⎦   ⎩ ⎭             (8-51)
                 N A , N B , and N K , different from   t+Δt N A  or   t+Δt N B ¸ are regular shape functions for a tri-
                                                     C
                                              C
              angular element. Therefore, for a triangular interface element, the three strain rates are
              given by:
                                                                            + t Δ t
                                                                              ⎧  •  ⎫ ⎫
                                                                              ⎪ U A ⎪
                     t+Δ t      ⎡                                          ⎤  ⎪ • ⎪
                        ⎧  •  ⎫                                               ⎪V ⎪
                                                                                 A
                        ⎪ ε nt ⎪  ⎢ − t+Δ t N C  0  − t+Δ t N C  0  1     0 ⎥  ⎪ • ⎪
                                                                                 B ⎪
                           ⎪
                        ⎪ • ⎪  ⎪  1 ⎢  A A  t+Δ       B    t+Δ             ⎥ ⎥  ⎪ ⎪U ⎪
                        ⎨ ε nn ⎬ =  ⎢  0  −  t N  C  0   −  t N  C  0     1 ⎥  ⎨  ⎬
                        ⎪  • ⎪  d ⎢ ⎢  ⎛ ∂ N ⎞  A  ⎛   ⎞       B  ⎛    ⎞   ⎥ ⎥  ⎪  •  ⎪
                        ⎪ε tt ⎪  ⎢ d ⎜ ⎜  A ⎟  0  d ⎜  ∂N B ⎟  0  d ⎜  ∂N  K ⎟  0 ⎥  ⎪ V  B ⎪
                        ⎩ ⎪  ⎭ ⎪  ⎣  ⎝  t ∂ ⎠     ⎝  ∂ ⎠          ⎝  ∂ ⎠   ⎦  ⎪  •  ⎪
                                                                     t
                                                     t
                                                                              ⎪ U  K ⎪
                                                                              ⎪  •  ⎪
                                                                                 K
                                                                              ⎩ ⎪V ⎭ ⎪
                                       + t Δ t
                                           •
                               1  + t Δ t  ⎧ ⎫
                             =     ⎡N ' ⎤ ⎦  ⎨ ⎬
                                          U
                                   ⎣
                               d         ⎩ ⎭
                                                                                 (8-52)
              8.3.4  Quadrilateral Interface Element
              Sometimes it would be more suitable to use quadrilateral elements to accommodate
              deformed configurations of interfaces. As shown in Figure 8.3b, relative displacement
              rates at time (t+Δt) between the upper and lower surfaces at any point in the element
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