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Laminar Reynolds analogy factor on a sharp flat plate at Mach 10.4Values measured on sharp flat plate in 10.4 Mach boundary layer induced pressure gradient, discussing effects of wall pressure and temperature gradients
Document ID
19700039493
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Stone, H. W.
Date Acquired
August 5, 2013
Publication Date
November 1, 1969
Subject Category
Aerodynamics
Accession Number
70A15609
Distribution Limits
Public
Copyright
Other

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