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EFFECTS OF CONTROLLED ROUGHNESS ON BOUNDARY-LAYER TRANSITION AT A MACH NUMBER OF 6.0Heat flow rate method used to investigate a hypersonic boundary layer transition on a smooth flat plate with a sharp leading edge
Document ID
19630024460
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Holloway, P. F.
Sterrett, J. R.
Date Acquired
August 1, 2013
Publication Date
January 1, 1953
Subject Category
Facilities, Research, And Support
Accession Number
63A20519
Distribution Limits
Public
Copyright
Other
Keywords
BOUNDARY LAYER TRANSITION
HYPERSONIC BOUNDARY LAYER

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