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Effect of vortices on delta wing lee-side heating at Mach 6Off-centerline heating on lee surface of supersonic delta wing with separation and vortex initiation at leading edge
Document ID
19700049880
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Whitehead, A. H., Jr.
Date Acquired
August 5, 2013
Publication Date
March 1, 1970
Subject Category
Aerodynamics
Accession Number
70A25996
Distribution Limits
Public
Copyright
Other

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