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Heat Transfer Measured in Free Flight on a Slightly Blunted 25 deg Cone-Cylinder-Flare Configuration at Mach Numbers up to 9.89Skin temperature and surface pressure of blunted cone-cylinder-flare configuration free flight test vehicle to hypersonic speeds
Document ID
19630010649
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Bond, Aleck C. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Lee, Dorothy B. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Rumsey, Charles B. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 26, 1958
Subject Category
Geophysics
Report/Patent Number
NACA-RM-L58G21
Report Number: NACA-RM-L58G21
Accession Number
63N20529
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SURFACE PRESSURE
CONE
BLUNT BODY
FLARED BODY
FREE FLIGHT
SKIN TEMPERATURE

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