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NASA NTRS · 19890054430

Upwind relaxation methods for the Navier-Stokes equations using inner iterations

Abstract

A supersonic and subsonic test problem is solved using an upwind line relaxation algorithm for the Navier-Stokes equations which employs inner iterations. In the supersonic test case, the inner iteration method was found to require only about 65 percent of the CPU time which was required by the most efficient line relaxation method without inner iterations. In the subsonic test case, poor matrix conditioning resulted in less efficiency than line relaxation methods employing a more conventional CPU-saving strategy.

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BibTeXRIS

Taylor, Arthur C., III, Hg, Wing-Fai, Walters, Robert W.. 1989-01-01. Upwind relaxation methods for the Navier-Stokes equations using inner iterations. https://ntrs.nasa.gov/citations/19890054430

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