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NASA NTRS · 19920062460

Parabolized reduced Navier-Stokes computational techniques

Abstract

A review is presented of methods in which composite or reduced Navier-Stokes (RNS) equations are treated with a pressure-gradient-based flux-vector splitting. The methods are similar to large Re asymptotic formulations, and streamwise diffusion terms are ignored in favor of an explicit deferred corrector based on higher-order diffusion terms. The methods can be used for 2D and 3D supersonic flows in which the effects of real gas are incorporated. Several examples of the procedure are given, and subsonic and supersonic flows are handled well with relaxation procedures that incorporate multigrid acceleration. Effective solutions are described for problems ranging from incompressible flows and supersonic flows to sharp shocks and reverse-flow capturing.

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BibTeXRIS

Rubin, Stanley G., Tannehill, John C.. 1992-01-01. Parabolized reduced Navier-Stokes computational techniques. https://ntrs.nasa.gov/citations/19920062460

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