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Boundary layer transition at hypersonic Mach numbers.Transition from laminar to turbulent boundary layer flow at hypersonic Mach numbers, noting measurement techniques
Document ID
19670039745
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Henderson, A., Jr.
Maddalon, D. V.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 67-130
Report Number: AIAA PAPER 67-130
Accession Number
67A18474
Distribution Limits
Public
Copyright
Other
Keywords
TRANSITION POINT
TURBULENT FLOW
REYNOLDS NUMBER
HYPERSONIC SPEED
LAMINAR BOUNDARY LAYER

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