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Hypersonic turbulent boundary-layer studies at cold wall conditions.Shock tunnel experiments with hypersonic turbulent boundary layer flow over flat plates with blunt and sharp leading edges and wall of expansion nozzle
Document ID
19670052225
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wallace, J. E.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Fluid Mechanics
Accession Number
67A30954
Funding Number(s)
CONTRACT_GRANT: AF 33/615/-1847
CONTRACT_GRANT: NSR-33-009-029
Distribution Limits
Public
Copyright
Other
Keywords
HYPERSONIC BOUNDARY LAYER
WALL TEMPERATURE
NOZZLE WALL
BOUNDARY LAYER FLOW
FLAT PLATE
TURBULENT BOUNDARY LAYER

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