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Recent experiments in hypersonic turbulent boundary layersHypersonic turbulent boundary layer experiments - skin friction, heat transfer, shear stress on flat plates and cones, and boundary layer velocity and thermal profiles on nozzle walls
Document ID
19650012964
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bertram, M. H. (NASA Langley Research Center Hampton, VA, United States)
Neal, L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-56335
Report Number: NASA-TM-X-56335
Accession Number
65N22565
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VELOCITY PROFILE
TURBULENT BOUNDARY LAYER
TURBULENT HEAT TRANSFER
SHEARING STRESS
FLAT PLATE

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