Page 240 - Fundamentals of The Finite Element Method for Heat and Fluid Flow
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                        Conservation of mass
                                                      ∂u 1
                                                                                           (7.197)
                                                          +  ∂u 2  = 0  CONVECTION HEAT TRANSFER
                                                      ∂x 1  ∂x 2
                        Conservation of momentum, x 1 component
                                                   1 ∂p                    ∂           ∂
                           ∂u 1    ∂u 1    ∂u 1           1 ∂τ 11  1 ∂τ 12
                               + u 1   + u 2   =−       +       +       −     (u u ) −   (u u )
                                                                                           1 2
                                                                               1 1
                            ∂t     ∂x 1    ∂x 2    ρ ∂x 1  ρ ∂x 1  ρ ∂x 2  ∂x 1       ∂x 2
                                                                                           (7.198)
                        Conservation of momentum, x 2 component
                           ∂u 2    ∂u 2    ∂u 2    1 ∂p   1 ∂τ 21  1 ∂τ 22  ∂          ∂
                               + u 1   + u 2   =−       +       +       −     (u u ) −   (u u )
                                                                               2 1
                                                                                           2 2
                            ∂t     ∂x 1    ∂x 2    ρ ∂x 2  ρ ∂x 1  ρ ∂x 2  ∂x 1       ∂x 2
                                                                                           (7.199)
                           All the terms of the above equations are very similar to the ones derived in the begin-
                        ning of this chapter, with averaged quantities appearing as the main variable. The major
                        difference, however, is due to the extra terms appearing in the equations, which are con-
                        cerned with the turbulent eddy process. These extra terms are normally modelled using
                        turbulence modelling techniques, in order to obtain time-averaged quantities. Therefore, to
                        model the turbulence, it is necessary to consider the widely used Boussinesq hypothesis,
                        namely,
                                                        ∂u i  ∂u j  2 ∂u k     2
                                       u u = τ R  = ν t   +     −      δ ij  − κδ ij       (7.200)

                                        i j    ij
                                                      ∂x j  ∂x i  3 ∂x k     3
                        where τ R  is the so-called Reynolds stress, ν t is the turbulent eddy viscosity and κ is the
                              ij
                        turbulent kinetic energy.
                           On substituting Equation 7.200 into the time-averaged momentum Equations 7.198 and
                        7.199, we obtain the final form of the averaged momentum equations as
                        Conservation of momentum, x 1 component
                            ∂u 1    ∂u 1   ∂u 1    1 ∂p    1 ∂τ 11  1 ∂τ 12  ∂τ 11 R  ∂τ 12 R
                               + u 1   + u 2   =−       +        +       +      +          (7.201)
                            ∂t      ∂x 1   ∂x 2    ρ ∂x 1  ρ ∂x 1  ρ ∂x 2   ∂x 1    ∂x 2
                        Conservation of momentum, x 2 component
                                                   1 ∂p                        R      R
                            ∂u 2    ∂u 2   ∂u 2            1 ∂τ 21  1 ∂τ 22  ∂τ 21  ∂τ 22
                               + u 1   + u 2   =−       +        +       +      +          (7.202)
                            ∂t      ∂x 1   ∂x 2    ρ ∂x 2  ρ ∂x 1  ρ ∂x 2   ∂x 1    ∂x 2
                           A closer examination of the time-averaged continuity Equation 7.197 and the momen-
                        tum Equations 7.201 and 7.202, shows that the extra parameters which remain and require
                        determination, are the turbulent eddy viscosity ν t and the turbulent kinetic energy κ.
                           The turbulent eddy viscosity may be calculated from several turbulence models. The
                        accuracy of such turbulence models can vary, but in this case a one-equation turbulence
                        model will be considered, which employs one transport equation in the calculation of the
                        turbulent eddy viscosity. The turbulent eddy viscosity relation is given as

                                                      ν t = C µ 1/4 1/2 l m                (7.203)
                                                              κ
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