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A computer program for calculating inviscid, adiabatic flow about blunt bodies traveling at supersonic and hypersonic speeds at angle of attackComputer program for determining inviscid flow around blunt bodies at supersonic and hypersonic speeds - users manual
Document ID
19710024194
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Barnwell, R. W. (NASA Langley Research Center Hampton, VA, United States)
Davis, R. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-2334
L-7771
Report Number: NASA-TM-X-2334
Report Number: L-7771
Accession Number
71N33670
Funding Number(s)
CONTRACT_GRANT: 136-13-05-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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