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NASA NTRS · 19870061806

Simple numerical method for predicting steady compressible flows

Abstract

The present numerical method for the solution of the isenthalpic form of the governing equations for compressible viscous and inviscid flows has its basis in the concept of flux vector splitting in its implicit form, and has been tested in the cases of several difficult viscous and inviscid configurations. An acceleration of time-marching to steady state is accomplished by implementing a multigrid procedure which effectively increases the convergence rate. The steady state results obtained are largely of good quality, and required only short computational times.

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BibTeXRIS

Von Lavante, E., Melson, N. Duane. 1987-01-01. Simple numerical method for predicting steady compressible flows. https://ntrs.nasa.gov/citations/19870061806

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