APRESSURE-BASED implicit procedure to solve steadystate Navier-Stokes equations is developed. A multistep pressure correction procedure with an implicit density treatment is used to establish the pressure and velocity fields. A multigrid relaxation scheme is used to solve the scalar matrices resulting from the finite-volume formulation. The algorithm is valid for all Mach number flows ranging from incompressible to supersonic flow regimes.
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Chae M. Rhie (1989) studied this question.
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