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A supersonic, three-dimensional code for flow over blunt bodies: User's manualA computer code is described which may be used to calculate the steady, supersonic, three-dimensional, inviscid flow over blunt bodies. The theoretical and numerical formulation of the problem is given (shock-capturing, downstream marching), including exposition of the boundary and initial conditions. The overall flow logic of the program, its usage, accuracy, and limitations are discussed.
Document ID
19800006790
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
January 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NEAR-TR-189
NASA-CR-3223
Accession Number
80N15049
Funding Number(s)
CONTRACT_GRANT: NAS1-15305
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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