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NASA NTRS · 19930061030

Euler solutions for blunt bodies using triangular meshes - Artificial viscosity forms and numerical boundary conditions

Abstract

A finite volume method is used to calculate compressible inviscid flows over blunt bodies using, in general, unstructured grids. Artificial viscosity forms are derived based on a simplified least squares procedure. The extra second order terms are consistent with the governing equations, hence a systematic treatment of the numerical boundary conditions can be easily implemented. A special treatment of blunt bodies may be required. The discrete equations are linearized and the resulting system is solved by a relaxation method. Preliminary results indicate that the effect of the numerical dissipation is minimal. For subsonic flows over smooth bodies, the solution is practically vorticity-free and the total pressure loss is of the same order as the truncation error. Finally, some extensions of the present method are briefly discussed.

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BibTeXRIS

Winterstein, R., Hafez, M.. 1993-01-01. Euler solutions for blunt bodies using triangular meshes - Artificial viscosity forms and numerical boundary conditions. https://ntrs.nasa.gov/citations/19930061030

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