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Heat-transfer and pressure distributions on a flat-face rounded-corner body of revolution with and without a flap at a Mach number of 8Heat transfer and pressure distributions on flat face rounded-corner body of revolution with and without flap control at hypersonic speeds and angles of attack from 0 deg to 45 deg
Document ID
19660024044
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jones, R. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1962
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-703
Report Number: NASA-TM-X-703
Accession Number
66N33334
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLAT SURFACE
ZERO ANGLE OF ATTACK
PRESSURE DISTRIBUTION
HEAT TRANSFER
FLAP CONTROL
BODY OF REVOLUTION
HYPERSONIC SPEED

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