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A time-dependent method for calculating supersonic blunt-body flow fields with sharp corners and embedded shock wavesTime-dependant method for calculating supersonic blunt body flow fields with sharp corners and embedded shock waves
Document ID
19710002058
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Barnwell, R. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1970
Subject Category
Fluid Mechanics
Report/Patent Number
L-7284
NASA-TN-D-6031
Report Number: L-7284
Report Number: NASA-TN-D-6031
Accession Number
71N11533
Funding Number(s)
CONTRACT_GRANT: 129-01-22-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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