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An evaluation of free-flight test data for aerodynamic heating from laminar, turbulent, and transitional boundary layers. Part II - The X-17 reentry bodyBlunt body reentry vehicle aerodynamic heating determination
Document ID
19660010795
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Murphy, J. D. (Itek Corp. Palo Alto, CA, United States)
Rubesin, M. W. (Itek Corp. Palo Alto, CA, United States)
Date Acquired
August 3, 2013
Publication Date
April 11, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-70931
Report Number: NASA-CR-70931
Accession Number
66N20084
Funding Number(s)
CONTRACT_GRANT: NAS7-216
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REENTRY VEHICLE
AERODYNAMIC HEATING
BLUNT BODY

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