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An entropy correction method for unsteady full potential flows with strong shocksAn entropy correction method for the unsteady full potential equation is presented. The unsteady potential equation is modified to account for entropy jumps across shock waves. The conservative form of the modified equation is solved in generalized coordinates using an implicit, approximate factorization method. A flux-biasing differencing method, which generates the proper amounts of artificial viscosity in supersonic regions, is used to discretize the flow equations in space. Comparisons between the present method and solutions of the Euler equations and between the present method and experimental data are presented. The comparisons show that the present method more accurately models solutions of the Euler equations and experiment than does the isentropic potential formulation.
Document ID
19860064838
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whitlow, W., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Hafez, M. M.
(California, University Davis, United States)
Osher, S. J.
(California, University Los Angeles, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 86-1768
Report Number: AIAA PAPER 86-1768
Accession Number
86A49576
Distribution Limits
Public
Copyright
Other

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