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Measurements of the Mach number and pressure on the afterbody of a blunt-nosed model in free flight at Mach numbers from 6.5 to 14Mach number and pressure measurements on afterbody of blunt-nose model in free flight at hypersonic speeds
Document ID
19660024048
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sommer, S. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-360
Report Number: NASA-TM-X-360
Accession Number
66N33338
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MACH NUMBER
BLUNT BODY
HYPERSONIC SPEED
AFTERBODY
PRESSURE MEASUREMENT

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