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Heat-transfer rates and ablation on a blunted cylinder-flare configuration in free flight up to a mach number of 8.98Heat-transfer rates and ablation on blunt flared cylinder in free flight at hypersonic and lower speeds
Document ID
19640017591
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Winters, C. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1964
Subject Category
Geophysics
Report/Patent Number
NASA-TN-D-2383
Report Number: NASA-TN-D-2383
Accession Number
64N27505
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC SPEED
CYLINDER
FREE FLIGHT
HEAT TRANSFER
ABLATION
FLARED BODY

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