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Heat-transfer measurements at Mach 8 on a flat plate with deflected trailing-edge flap with effects of transition includedHeat transfer measurements on flat plate with trailing edge flap in hypersonic flow
Document ID
19700023517
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Johnson, C. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1970
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-5899
L-6349
Report Number: NASA-TN-D-5899
Report Number: L-6349
Accession Number
70N32828
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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