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A description of numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodiesNumerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodies
Document ID
19650021355
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Inouye, M. (NASA Ames Research Center Moffett Field, CA, United States)
Lomax, H. (NASA Ames Research Center Moffett Field, CA, United States)
Rakich, J. V. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2970
Report Number: NASA-TN-D-2970
Accession Number
65N30956
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AXISYMMETRIC FLOW
COMPUTER PROGRAM
SUPERSONIC FLOW
BLUNT BODY

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