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Two-Dimensional Elasticity                                                  125



                                                   v 3
                                                3
                                             (x , y )   u 3
                                              3
                                                3
                                                  v
                                                               v 2
                                          v 1  (x, y)  u       2
                                   y                                u 2
                                        1     u              (x , y )
                                                              2
                                                                2
                                       (x , y )  1
                                          1
                                        1
                                          x
            FIGURE 4.8
            Linear triangular element (T3).


            in the x and y directions). The displacements u and v are assumed to be linear functions
            within the element, that is

                                   u =  b +  bx +  by,  v =  b +  bx +  by             (4.14)
                                       1   2    3        4   5    6

            where b  (i = 1, 2, …, 6) are constants. From these, the strains are found to be
                   i
                                     ε= b 2 ,  ε= b 6 ,                                (4.15)
                                      x        y      γ xy  = b 3  + b 5

            which are constant throughout the element. Thus, we have the name “constant strain tri-
            angle” (CST).
              Displacements given by Equation 4.14 should satisfy the following six equations:

                                           u 1 =  b 1 +  bx +  by
                                                    21
                                                         31
                                           u 2 =  b 1 +  bx +  by
                                                    22
                                                         32

                                           v 3 =  b 4 +  bx +  by
                                                    53    63
              Solving these equations, we can find the coefficients b , b , …, and b  in terms of nodal
                                                              1
                                                                          6
                                                                 2
            displacements and coordinates. Substituting these coefficients into Equation 4.14 and rear-
            ranging the terms, we obtain
                                                                     u 
                                                                     1
                                                                       
                                                                      v 1 
                                u    N 1  0  N 2   0    N 3   0    u 2 
                                                                       
                                                                    
                                 =                                               (4.16)
                                v
                                     0  N 1   0    N 2   0   N 3    v 2 
                                                                     u 3 
                                                                      
                                                                      v 3  
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