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Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5 deg half-angle cone at Mach 8Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on 5 degree half-angle cone at Mach 8
Document ID
19690005540
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Stainback, P. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4961
Report Number: NASA-TN-D-4961
Accession Number
69N14872
Funding Number(s)
CONTRACT_GRANT: 129-01-08-38-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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