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A simple integral method for the calculation of real-gas turbulent boundary layers with variable edge entropySimple integral method for calculating real gas turbulent boundary layers with variable edge entropy and flight calculations showing effect of nose bluntness at 6.09 km/sec
Document ID
19710018538
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Boney, L. R. (NASA Langley Research Center Hampton, VA, United States)
Johnson, C. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
L-7415
NASA-TN-D-6217
Report Number: L-7415
Report Number: NASA-TN-D-6217
Accession Number
71N28014
Funding Number(s)
CONTRACT_GRANT: 129-01-20-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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