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134   Ch a p t e r  Fiv e


                 By these considerations, it is assumed that the effective aggregate is a linearly elastic
              material observing the following constitutive equation:

                                           τ =  λε  + 2 με                       (5-25)
                                            sij  skk   sij
                 Where l  and m  are the Lame’s constants; t sij  and e sij are the stress and the strain ten-
              sor in the real material, and the subscript “s” represents solids.
                 It is assumed that the air voids behave as an ideal compressible gas observing the
              following constitutive equation:

                                              τ =−  δ p                          (5-26)
                                               aij   ij
                                              p = γ  RT                          (5-27)
                                                  a
                 Where R = the universal gas constant, T = the absolute temperature, g a  = the density
              of air, and t aij  = the stress in the air; the subscript a represents air.
                 The stress calculated from the above two equations is the actual stress in the mate-
              rial. It is related to the partial stress by the following equation:

                                              σ =  φτ                            (5-28)
                                               sij  sij
                                                     )
                                            σ = (1  − φ τ                        (5-29)
                                             aij       aij
              Momentum interaction
              With the consideration of static loading, Equation 5-22 can be simplified as:
                                      p =−ξγ   grad +φ ξ γ  gradφ                (5-30)
                                       s    11  s     12  a

                                      p =−ξγ   grad +φ ξ γ  gradφ                (5-31)
                                       a    21  s     22  a
              Boundary conditions
              There are many methods proposed to handle the boundary condition problem (Rajago-
              pal, 1996). Krishnan and Rao (2000) also followed Rajagopal’s method. The basic idea is
              to use the relation that the area fraction is equal to the volume fraction and distribute
              the mixture surface traction to the partial surface traction of constituents according to
              their area fraction.
                                              σ n =  t                           (5-32)
                                               α  s  α
                                               t =  φ  t                         (5-33)
                                               α   α
                 Where s a  is the partial stress; n s  is the normal to the surface, and t a  is the partial trac-
              tion.
                 By the distribution proportions expressed in Equation 5-33, it is easy to show that
               N
                     N
              ∑  t α ∑  φ = t . Formally, it satisfies the requirements. However, it should be noted
                   =
                         t
                         α
              α=1    α=1
              that Equation 5-33 might not hold universally. For example, the shear components of
              the surface traction cannot be allocated to the air constituent at all. In general, bound-
              ary conditions might be case dependent. In the two-constituent situation (solids and
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