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Euler solutions for blunt bodies using triangular meshes - Artificial viscosity forms and numerical boundary conditionsA 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.
Document ID
19930061030
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Winterstein, R.
(NASA Ames Research Center Moffett Field, CA, United States)
Hafez, M.
(California Univ. Davis, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Computational Fluid Dynamics Conference, 11th, Orlando, FL, July 6-9, 1993, Technical Papers. Pt. 1 (A93-44994 18-34)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-3333
Accession Number
93A45027
Funding Number(s)
CONTRACT_GRANT: NCA2-663
CONTRACT_GRANT: NCA2-644
Distribution Limits
Public
Copyright
Other

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