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A supersonic three-dimensional code for flow over blunt bodies: Program documentation and test casesThe use of a computer code for the calculation of steady, supersonic, three dimensional, inviscid flow over blunt bodies is illustrated. Input and output are given and explained for two cases: a pointed code of 20 deg half angle at 15 deg angle of attack in a free stream with M sub infinite = 7, and a cone-ogive-cylinder at 10 deg angle of attack with M sub infinite = 2.86. A source listing of the computer code is provided.
Document ID
19800008768
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chaussee, D. S. (Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Mcmillan, O. J. (Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3224
NEAR-TR-194
Report Number: NASA-CR-3224
Report Number: NEAR-TR-194
Accession Number
80N17028
Funding Number(s)
CONTRACT_GRANT: NAS1-15305
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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