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Improvements and applications of a streamwise upwind algorithmAn improved streamwise upwind algorithm has been used to study conical flow fields. In the present method, additional terms have been introduced in the cross-flow direction to prevent solution decoupling in supersonic flows, and the local Mach number is taken into account in order to evaluate the rotated differencing. It is found that the formula captures oblique shock waves in the same manner as Roe's (1986) formula, has good convergence properties, and accurately computes shear flows.
Document ID
19890054433
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Obayashi, Shigeru
(NASA Ames Research Center Moffett Field, CA, United States)
Goorjian, Peter M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 89-1957
Report Number: AIAA PAPER 89-1957
Meeting Information
Meeting: AIAA Computational Fluid Dynamics Conference
Location: Buffalo, NY
Country: United States
Start Date: June 13, 1989
End Date: June 15, 1989
Accession Number
89A41804
Distribution Limits
Public
Copyright
Other

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