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A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flowComputational method for surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow
Document ID
19690000884
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Jackson, C. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Sawyer, W. C. (NASA Langley Research Center Hampton, VA, United States)
Smith, R. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4865
Report Number: NASA-TN-D-4865
Accession Number
69N10215
Funding Number(s)
CONTRACT_GRANT: 722-01-00-02-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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