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Boundary layers and hypersonic inlet flow fields.Shock wave boundary layer interactions and shear flow regimes in hypersonic inlet flows
Document ID
19660055157
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gallo, W. F.
Gnos, A. V.
Latham, E. A.
Watson, E. C.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 66-606
Report Number: AIAA PAPER 66-606
Accession Number
66A34447
Distribution Limits
Public
Copyright
Other
Keywords
FLOW SEPARATION
INLET FLOW
HYPERSONIC FLOW
TRANSITION LAYER
SHOCK WAVE
BOUNDARY LAYER

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