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Numerical simulation of the hypersonic flow around lifting vehiclesA method of solving the viscous hypersonic flow field around realistic configurations is presented. The numerical procedure for generating the required finite difference grid and the two-factored implicit flow solver are described. Results are presented for the shuttle orbiter and a generic wing-body configuration at hypersonic Mach numbers.
Document ID
19880003852
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rizk, Yehia (Sterling Federal Systems, Inc. Palo Alto, Calif., United States)
Chaussee, Denny (NASA Ames Research Center Moffett Field, CA, United States)
Steger, Joseph (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1987
Publication Information
Publication: AGARD, Aerodynamics of Hypersonic Lifting Vehicles
Subject Category
Aerodynamics
Accession Number
88N13234
Distribution Limits
Public
Copyright
Other
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