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NASA NTRS · 19920046929

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

Abstract

A subsonic and a supersonic problem are respectively treated by an upwind line-relaxation algorithm for the Navier-Stokes equations using inner iterations to accelerate steady-state solution convergence and thereby minimize CPU time. While the ability of the inner iterative procedure to mimic the quadratic convergence of the direct solver method is attested to in both test problems, some of the nonquadratic inner iterative results are noted to have been more efficient than the quadratic. In the more successful, supersonic test case, inner iteration required only about 65 percent of the line-relaxation method-entailed CPU time.

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BibTeXRIS

Taylor, Arthur C., III, Ng, Wing-Fai, Walters, Robert W.. 1992-03-01. Upwind relaxation methods for the Navier-Stokes equations using inner iterations. https://ntrs.nasa.gov/citations/19920046929

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