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Cone transitional boundary-layer structure at Me = 14.Experimental results suggest that the boundary-layer mean profiles in hypersonic flows may be highly transitional in the outer part of the boundary layer before the transition process is detected at the surface. Means of determining the initial location where the transition process begins in the outer part of the boundary layer are considered.
Document ID
19720049171
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Fischer, M. C.
Weinstein, L. M.
(NASA Langley Research Center Hypersonic Vehicles Div., Hampton, Va., United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Publication Information
Publication: AIAA Journal
Volume: 10
Subject Category
Aerodynamics
Accession Number
72A32837
Distribution Limits
Public
Copyright
Other

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