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Experimental investigation of leading-edge shock impingement and interaction heating on a 1/80 scale model of a NASA straight wing orbiter configuration at Mach numbers 8 and 16Leading edge shock impingement and interaction heating on scale model straight wing orbiter
Document ID
19710025720
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rogers, C. E. (State Univ. of New York Buffalo, NY, United States)
Date Acquired
August 6, 2013
Publication Date
August 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
CAL-AA-2977-Y-1
NASA-CR-115159
Report Number: CAL-AA-2977-Y-1
Report Number: NASA-CR-115159
Accession Number
71N35196
Funding Number(s)
CONTRACT_GRANT: NAS9-11084
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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