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Transition to turbulence in hypersonic flowAn outline of the project and recent progress toward the study of transition in hypersonic boundary layers is given. Aspects of the numerical method and the results of test computations are presented. At present the laminar flows over a flat plate have been computed for M less than or equal to 5.
Document ID
19920020918
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Vandervegt, J. J. W. (Stanford Univ. CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1990
Publication Information
Publication: Annual Research Briefs, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92N30161
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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