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Effects of angle of attack and bluntness on laminar heating-rate distributions of a 15 deg cone at a Mach number of 10.6Laminar heating rate from wind tunnel tests using angle of attack and Reynolds number
Document ID
19690028226
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cleary, J. W. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1969
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-5450
Report Number: NASA-TN-D-5450
Accession Number
69N37604
Funding Number(s)
CONTRACT_GRANT: 129-01-03-10-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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