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SUPERSONIC FLOW IN THE REGION OF AN ANGULAR LEDGEShock wave and boundary layer interaction in supersonic flow in angular ledge region
Document ID
19630002392
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ionov, V. P. (Academy of Sciences (USSR) Moscow, Ussr)
Date Acquired
August 1, 2013
Publication Date
January 1, 1962
Subject Category
Facilities, Research, And Support
Accession Number
63N12268
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC FLOW
BOUNDARY LAYER
SHOCK WAVE
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