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Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners, including a program description and listingFORTRAN program for approximate calculation of supersonic ideal gas flow past blunt bodies with sonic corners
Document ID
19680015621
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
South, J. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4563
Report Number: NASA-TN-D-4563
Accession Number
68N25093
Funding Number(s)
CONTRACT_GRANT: 129-01-03-06-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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