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Analysis of hypersonic pressure and heat transfer tests on a flat plate with a flap and a delta wing with body, elevons, fins, and rudders Final reportHypersonic boundary layer separation and flow field interference analysis during Dyna-Soar space glider testing
Document ID
19660026817
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Giles, H. L. (Boeing Co. Seattle, WA, United States)
Thomas, J. W. (Boeing Co. Seattle, WA, United States)
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-536
Report Number: NASA-CR-536
Accession Number
66N36107
Funding Number(s)
CONTRACT_GRANT: NAS1-4301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
X-20 AIRCRAFT
FLOW FIELD
HYPERSONIC BOUNDARY LAYER

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