Page 128 - Introduction to Computational Fluid Dynamics
P. 128

P1: IWV
                                                                                   May 20, 2005
                           CB908/Date
                                        0 521 85326 5
            0521853265c05
                        5.1 INTRODUCTION
                        ρ and 
 were not functions of scalar  s then the flow equations for   = u 1 , u 2 12:28 107
                        will be independent of the scalar transport equations. This is the first reason for
                        distinguishing the flow-field equations from other scalar transport equations. To
                        appreciate the second reason, we first set out the equations governing the flow field
                        (the Navier–Stokes equations):
                                        ∂(ρ)   1 ∂             1 ∂
                                             +       {r ρ u f1 } +   {r ρ u f2 } = 0,       (5.3)
                                         ∂t    r ∂x 1          r ∂x 2
                            ∂(ρ u 1 )  1 ∂              1 ∂
                                   +       {r ρ u f1 u 1 } +  {r ρ u f2 u 1 }
                              ∂t      r ∂x 1            r ∂x 2

                                        ∂p    1 ∂         ∂u 1    1 ∂         ∂u 1
                                   =−       +        r µ eff   +        r µ eff    + S u1 ,  (5.4)
                                        ∂x 1  r ∂x 1      ∂x 1    r ∂x 2      ∂x 2
                            ∂(ρ u 2 )  1 ∂              1 ∂
                                   +       {r ρ u f1 u 2 } +  {r ρ u f2 u 2 }
                              ∂t      r ∂x 1            r ∂x 2
                                        ∂p    1 ∂         ∂u 2     1 ∂        ∂u 2
                                   =−       +        r µ eff   +         r µ eff   + S u2 .  (5.5)
                                        ∂x 2  r ∂x 1      ∂x 1    r ∂x 2      ∂x 2
                           A few comments having a bearing on the solution strategy are now in order.

                        1. In Equations 5.3–5.5, there are three unknowns (u 1 , u 2 , and p). Therefore, the
                           equation set is solvable.
                        2. In boundary layer flows, the pressure gradient is specified (external flows) or is
                           evaluated via the overall duct mass flow rate balance (internal flows). In elliptic
                           flows, however, ∂p/∂x 1 and ∂p/∂x 2 are not a priori known.
                        3. Thus, if we regard Equation 5.4 as the determinant of u 1 field and Equation 5.6
                           as the determinant of u 2 field, then the pressure field can be established only via
                           the mass conservation equation (5.3). The situation is somewhat similar to the
                           case of internal boundary layer flows but is not as straightforward.
                        4. The suffix f is attached to velocities satisfying the mass conservation equa-
                           tion. The velocity field without suffix f may or may not satisfy mass conserva-
                           tion directly although, in a continuum, it is expected that the u i and u fi fields
                           are identically overlapping and, therefore, the former must also satisfy mass
                           conservation.
                        5. The reader may find this distinction between the u i and u fi fields somewhat
                           unfamiliar. This is because most textbooks a priori assume a fluid continuum.
                           Numerical solutions are, however, developed in a discretised space and the
                           distinction mentioned here becomes relevant. This will become clear in a later
                           section.

                           These points reveal the fact that there is no explicit differential equation for
                        determination of the pressure field with p (or its variant) as the dependent variable.
   123   124   125   126   127   128   129   130   131   132   133