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Method for predicting compressible turbulent boundary layers in adverse pressure gradientsMethod for predicting compressible turbulent boundary layers in adverse pressure gradients applied to hypersonic air breathing propulsion
Document ID
19710022734
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pinckney, S. Z. (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-TM-X-2302
L-6802
Report Number: NASA-TM-X-2302
Report Number: L-6802
Accession Number
71N32210
Funding Number(s)
CONTRACT_GRANT: 764-75-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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