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Critical review of experimental heat transfer coefficients and temperature distributions in turbulent boundary layers at supersonic and hypersonic flowHeat transfer coefficients and temperature distributions in turbulent boundary layers at supersonic and hypersonic flow
Document ID
19670022228
Acquisition Source
Legacy CDMS
Document Type
Technical Translation (TT)
Authors
Rotta, J. C.
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TT-F-10905
Report Number: NASA-TT-F-10905
Accession Number
67N31557
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
TURBULENT BOUNDARY LAYER
HEAT-TRANSFER COEFFICIENT
TEMPERATURE DISTRIBUTION
SUPERSONIC FLOW
HYPERSONIC FLOW

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