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Hypersonic turbulent boundary layer studies at cold wall conditionsSkin friction and heat transfer rate in hypersonic turbulent boundary layer flow over flat plates and cold nozzle walls
Document ID
19680018055
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wallace, J. E. (State Univ. of New York Buffalo, NY, United States)
Date Acquired
August 4, 2013
Publication Date
February 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-82425
Report Number: NASA-CR-82425
Meeting Information
Meeting: 1967 HEAT TRANSFER AND FLUID MECH. INST.
Location: LA JOLLA, CA
Country: UNITED STATES
Start Date: June 19, 1967
End Date: June 21, 1967
Accession Number
68N27527
Funding Number(s)
CONTRACT_GRANT: NSR-33-009-029
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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