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Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8
Document ID
19930084472
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Crawford, Davis H
Mccauley, William D
Date Acquired
August 16, 2013
Publication Date
July 1, 1956
Report/Patent Number
NACA-TN-3706
Report Number: NACA-TN-3706
Accession Number
93R13762
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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