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Analysis of hypersonic pressure and heat transfer tests on delta wings with laminar and turbulent boundary layers Final reportHypersonic pressure and heat transfer tests on delta wings with laminar and turbulent boundary layers
Document ID
19660026816
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Doyle, L. B. (Boeing Co. Seattle, WA, United States)
Fitzsimmons, H. D. (Boeing Co. Seattle, WA, United States)
Nagel, A. L. (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-535
Accession Number
66N36106
Funding Number(s)
CONTRACT_GRANT: NAS1-4301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBULENT BOUNDARY LAYER
HYPERSONIC WIND TUNNEL
DELTA WING
LAMINAR BOUNDARY LAYER
HEAT TRANSFER

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