Page 88 - gas transport in porous media
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81
                           Chapter 6: Conservation Equations
                           enthalpy per unit mass is defined by
                                                     ρ A h A = ρ A e A + p A             (6.58)
                           in which p A is the partial pressure of species A. This is defined according to

                                                        2  ∂e A
                                                  p A = ρ                                (6.59)
                                                        A
                                                           ∂ρ A  s, ρ B , ρ C , ...
                            in which s is the total entropy per unit mass of the mixture. Following the approach
                           used for a Stokesian fluid, the species stress tensor is decomposed according to
                                                      T A =−I p A + τ A                  (6.60)
                           and Eqs. (6.58) through (6.60) can be used in Eq. (6.57) to obtain
                                                                    B=N
                                  ∂
                                    (ρ A h A ) +∇ · (ρ A h A v A ) =−∇ · q A +  Q AB     (6.61)
                                  ∂t
                                                                    B=1
                                                          +∇v A : (−I p A ) +∇v A : τ A + r A e A
                                                            ∂p A
                                                          +     +∇ · (p A v A )
                                                             ∂t
                           We now make use of the definitions,
                                             A=N             A=N            A=N

                                        ρh =     ρ A h A ,  q =  q A ,  p =    p A       (6.62)
                                             A=1             A=1            A=1
                           along with Axiom III, and sum Eq. (6.61) over all species to obtain
                                                A=N                  A=N
                                     ∂
                                       (ρh) +∇ ·    ρ A h A v A =−∇ · q +  ∇v A : (− I p A )  (6.63)
                                     ∂t
                                                A=1                   A=1
                                                               A=N          A=N

                                                             +    ∇v A : τ A +  r A e A
                                                               A=1          A=1
                                                                       A=N
                                                               ∂p
                                                             +    +∇ ·    p A v A
                                                               ∂t
                                                                       A=1
                           On the basis of Eqs. (6.6), (6.26), and (6.54), and the velocity decomposition given
                           by Eq. (6.37) we can prove that
                                                 A=N       A=N

                                                                 1  2
                                                     r A e A +  r A  u = 0               (6.64)
                                                                 2  A
                                                 A=1       A=1
                           In addition, we can use the velocity decomposition given by Eq. (6.37) along with
                           the stress decomposition given by Eq. (6.60) to obtain the following results:
                                              A=N                A=N

                                                  ρ A h A v A = ρhv +  ρ A h A u A       (6.65)
                                              A=1                A=1
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