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NASA NTRS ยท 19790021971

Test problems for inviscid transonic flow

Abstract

Solving of test problems with the TRANDES program is discussed. This method utilizes the full, inviscid, perturbation potential flow equation in a Cartesian grid system that is stretched to infinity. This equation is represented by a nonconservative system of finite difference equations that includes at supersonic points a rotated difference scheme and is solved by column relaxation. The solution usually starts from a zero perturbation potential on a very coarse grid (typically 13 by 7) followed by several grid halvings until a final solution is obtained on a fine grid (97 by 49).

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BibTeXRIS

Carlson, L. A.. 1979-09-01. Test problems for inviscid transonic flow. https://ntrs.nasa.gov/citations/19790021971

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