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A time-dependent method for calculating supersonic angle-of-attack flow about axisymmetric blunt bodies with sharp shoulders and smooth nonaxisymmetric blunt bodiesHypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based on time dependent finite difference theory and method of characteristics
Document ID
19710021731
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
August 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-6283
L-7593
Report Number: NASA-TN-D-6283
Report Number: L-7593
Accession Number
71N31207
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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