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FREE-FLIGHT HEAT-TRANSFER INVESTIGATION AT SUPERSONIC SPEEDS OF TWO SLENDER CONE-CYLINDER BODIES AT AN ANGLE OF ATTACK OF 8 DEG WITH ONE BODY ROTATINGSupersonic free flight heat transfer study of two cone cylinder bodies at angle of attack of 8-deg with one body rotating
Document ID
19630004014
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Falanga, R. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1959
Subject Category
Geophysics
Report/Patent Number
NASA-MEMO-12-31-58L
Report Number: NASA-MEMO-12-31-58L
Accession Number
63N13890
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROTATING BODY
FREE FLIGHT
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