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An analytical study of separated flows induced by shock wave - Boundary layer interactionAnalytical study of separated flows induced by shock wave-boundary layer interaction
Document ID
19660027557
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Holden, M. S.
Date Acquired
August 3, 2013
Publication Date
October 1, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-600
Report Number: NASA-CR-600
Accession Number
66N36847
Funding Number(s)
CONTRACT_GRANT: NAS5-3976
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SEPARATED FLOW
BOUNDARY LAYER
SHOCK WAVE INTERACTION

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