Page 259 - Mechanics of Asphalt Microstructure and Micromechanics
P. 259

F inite Element Method and Boundar y Element Method   251


                 The strains can be represented as:
                    ⎧  ∂  ⎫
                    ⎪  ,0  ⎪
                    ⎪  x ∂  ⎪
                    ⎪  ∂  ⎪
                 L = ⎨ ,0  ⎬
                    ⎪   y ∂  ⎪
                    ⎪  ∂  ∂  ⎪
                    ⎪  ,  ⎪
                    ⎩  y ∂  x ∂  ⎭
                    ⎧ β ,, β ,, β ,0  ⎫
                            0
                        0
                    ⎪  i  j   k    ⎪ ⎪
                    ⎪
                    ⎨
                             0
                         0
                 B = 0  γ ,, , γ , , γ k  ⎬
                        i
                            j
                    ⎪              ⎪
                       ,,
                              ,
                            ,
                    ⎩ ⎪ γβ γ β γ ,β k ⎭ ⎪
                             j
                      i
                                k k
                         i
                           j
                 Obviously, for a fixed triangle, B is a constant matrix (only related to the coordinates
              of the three nodes). In other words, the strains are constant in the element if the linear
                                                             T
                                                      v
                                                          ,
              interpolation functions are used (e = B  (, , , ,u v  ) ). Typically, for higher order
                                                    u
                                               uv
                                                i  i  j  j  k  k
              polynomial interpolation functions, the strains in the element are not constant.
                 Step 3: This is actually the process to obtain the element stiffness matrix and the
              equivalent node forces due to the boundary forces and the body forces.
                 K =   e ∫  B CBdΩ
                         T
                   e
                      Ω
                         ⎧        ⎫
                         ⎪1 ν ,, 0  ⎪
                 C =  E  ⎪ ⎨ 10   ⎪
                                  ⎬
                          ν,,
                    1 −ν 2  ⎪  −ν ⎪
                         ⎪00 ,,  1  ⎪
                         ⎩     2  ⎭
                                                     e
                 Apparently B CB is a constant matrix and K  is a 6   6 symmetric matrix.
                            T
                  S ∫
                         T
                 F    Γ  e  N d τ Γ: equivalent forces due to the surface tractions
                  e
                  B ∫
                         T
                  e
                 F    Ω  e  N bdΩ: equivalent forces due to distributed body forces
                   e ∫  NbdΩ
                     T
                  Ω
                 ⎡ N ,,  N ,,  N ,0⎤
                     0
                         0
                 ⎢  i   j    k  ⎥
                           0
                      0
                 ⎣  , 0 ⎢  N , , N , , N ⎥
                              k ⎦
                     i
                          j
                    ⎧0   ⎫ ⎪
                 b = ⎨   ⎬
                    ⎩ −ρ g ⎭
                 Nb = ( , −ρ gN ,, −ρ gN ,, −ρ gN ) T
                                      0
                      0
                              0
                             i      j       k
                  e
                                         3
                                           0
                      0
                 F = (, −ρ gAh/ , , −ρ gAh/ , , −ρ gAh/ ) T
                                0
                              3
                                                    3
                  B
                          τ
                 F =   N dΓ
                         T
                  e
                  S ∫ Γ e
                 In this special case, the only non-zero component is –P at Node 24.
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