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HEAT-TRANSFER MEASUREMENTS OF TWO WING-BODY COMBINATIONS AT 8 DEG ANGLE OF ATTACK FROM A FLIGHT TEST FOR MACH NUMBERS TO 4.86 AND REYNOLDS NUMBERS TO 19.2 X 10 SUPER 6Heat transfer measurements from flight test of two wing-body combinations at mach numbers to 4.86
Document ID
19630002622
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Speegle, K. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1958
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-10-25-58L
Report Number: NASA-MEMO-10-25-58L
Accession Number
63N12498
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBULENT FLOW
AERODYNAMIC HEAT TRANSFER
HEAT TRANSFER
BODY-WING COMBINATION
AERODYNAMIC HEATING
FLIGHT TEST
FREE FLIGHT
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