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Vortex-induced heating to a cone-cylinder body at Mach 6Presented data on vortex-induced heating in a cone-cylinder body at Mach 6 show that the most severe heating need not occur as a result of the interaction of the primary vortices with the lee surface, even though this interaction produces a large, well-defined featherline oil smear. It is pointed out that the severity of vortex-induced heating is extremely sensitive to Reynolds number and geometry and that there exists a 'threshold Reynolds number' below which vortex-induced heating decreases abruptly.
Document ID
19740038649
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hefner, J. N.
(NASA Langley Research Center Hypersonic Vehicles Div., Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
February 1, 1974
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 11
Subject Category
Aerodynamics
Accession Number
74A21399
Distribution Limits
Public
Copyright
Other

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