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NASA NTRS ยท 19860036297

Finite difference simulation of unsteady interactive flows

Abstract

The development of time-dependent numerical simulations of unsteady interactive flows of an aerodynamic nature is reviewed with emphasis on compressible flows at flight Reynolds numbers and noniterative schemes based on Navier-Stokes equations. The importance of writing the equations in strong conservation-law form for a generalized body-oriented coordinate system is pointed out. The discussion covers time and length scales and numerical methods currently in use. Some computed results are presented and compared with experimental data.

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BibTeXRIS

Deiwert, G. S.. 1984-01-01. Finite difference simulation of unsteady interactive flows. https://ntrs.nasa.gov/citations/19860036297

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