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Effect of Reynolds number and boundary-layer transition location on shock-induced separationEffect of Reynolds number and boundary layer transition location on shock induced separation
Document ID
19690019331
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Blackwell, J. A., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 5, 2013
Publication Date
September 1, 1968
Publication Information
Publication: AGARD TRANSONIC AERODYN. SEP. 1968 (SEE N69-28694 15-01)
Subject Category
Aerodynamics
Accession Number
69N28709
Distribution Limits
Public
Copyright
Other
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