Page 300 - Introduction to Computational Fluid Dynamics
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                        APPENDIX A. DERIVATION OF TRANSPORT EQUATIONS
                        5. Inincompressibleflows,thedensityρ m isexternallyspecifiedasaconstantorasa  13:6 279
                           function of temperature and the sum of partial densities of mixture components.
                           In compressible flow, however, the density is recovered from an equation of
                                                                                       4
                           state. Thus, according to the law of corresponding states, for reduced pressure
                            p r < 0.5 and reduced temperature T r > 1.5, the density is calculated from the
                           perfect gas relation
                                                            p     pM g
                                                    ρ m =      =      ,                   (A.17)
                                                          R g T   R u T
                           where M g is the molecular weight of the gas and R u is the universal gas constant.



                        A.4 Equation of Mass Transfer
                        The conservation of mass for species k of the mixture is stated as

                                                                             ˙
                                                      ˙
                          Rate of accumulation of mass (M k,ac ) = Rate of mass in (M k,in )
                                                                                ˙
                                                              − Rate of mass out (M k,out )
                                                              + Rate of generation within CV (R k ).

                           To apply this principle, let ρ k be the density of the species k in a fluid mixture
                                                                                2
                        of density ρ m . Similarly, let N i,k be the mass transfer flux (kg/m -s) of species k in
                        the i direction. Then

                                  ∂(ρ k  V )
                           ˙
                          M k,ac =         ,
                                     ∂t
                           ˙                                                       ,
                           M k,in = N 1,k  x 2  x 3 | x 1  + N 2,k  x 3  x 1 | x 2  + N 3,k  x 1  x 2 | x 3
                           ˙
                          M k,out = N 1,k  x 2  x 3 | x 1 + x 1  + N 2,k  x 3  x 1 | x 2 + x 2  + N 3,k  x 1  x 2 | x 3 + x 3 .
                           Dividing each term by  V and letting  x 1 , x 2 , x 3 → 0, we get

                                         ∂(ρ k )  ∂(N 1,k )  ∂(N 2,k )  ∂(N 3,k )
                                              +         +        +         = R k .        (A.18)
                                          ∂t      ∂x 1      ∂x 2     ∂x 3

                        Now, the total mass transfer flux N i,k is the sum of convective flux due to bulk fluid
                        motion (with each species having the same velocity as the bulk fluid) and diffusion

                        flux (m ). Thus,
                               i,k

                                                    N i,k = ρ k u i + m .                 (A.19)
                                                                   i,k


                        4  Reduced pressure and temperature are defined as p r = p/p cr and T r = T/T cr , where the suffix cr
                          stands for the critical point.
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