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332                                 11.  Incompressible  Navier-Stokes  Equations



            Substituting  Eq.  (11.4.4)  into  Eq.  (11.4.3)  and  noting  that  the  D's  are  vec-
         tors,  leads  to  the  following  delta  form

                                             n
                                _/_       (dR\    r       n
                                               AD       -R                 (11.4.5)
                                    +
                                AT      \dDJ
                                             X
                                           n
                        n+l
         where  AD n  =  D -D n  and  AT  =  T + -T n  and  /  is the  3 x 3 identity  matrix,
         or  in  compact  form
                                      'BAD 71  =  -R n                     (11.4.6)
         where
                                         _/_    (dR\ n                    (11.4.7)
                                         zi7  +  \dD)


                                  t
         11.4.2  Discretization  of he  Convective  Fluxes
         The  analysis  in  Section  11.2  showed  that  the  system  is  hyperbolic,  and  the
         upwind  method  is applied  as discussed  in  Section  5.5. The  Jacobian  matrices  of
         the  convective  flux  E  and  F  are

                              o  p   o                 0  0   (3
                  A    9  E                B -  9 F  -
                 A            1  2u  0     B           0  v   u           (11.4.8)
                   =  0D  =                -dD~
                              0  v   u                 1   0  2v
         and  the  eigenvalues  A  and  eigenvectors  X  of  A  and  B  can  be  written  as
                               iW
                                                    u    0       0
             Ai  =  X^AXi  =         ,(1)           0  u  +  c\  0
                                          A  (i)    0    0        u-c\\
                                (2)
                               A                    v    0       0
                    L                 (2)
             A 2~-= X^ BX 2  =       A              0  v  +  c 2  0
                                           (2)      0    0
                                          A                      v-c 2    (11.4.9)
                                          6
                               o        Clp   "       - Clp   •
                   Xl          0   u(ci  +  u)  +  /3  u(ci-u)  +  P
                      = Wr
                              \_2f3  v{c\  +  u)      v(c\—u)
                              '  0       C20           -C2/3
                  X2 =        -2/3         +  v)         -  v)
                        W  2    0   v(c 2  + v)  + (3  v(c 2-v)  +  (3}
                                      u(c 2
                                                     u(c 2
        where
                                      c\                                (11.4.10a)

        and
                                                                        (11.4.10b)
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