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Bluntness and boundary layer displacement effects on hypersonic inlet flow fields.Bluntness and boundary layer displacement effects on air breathing engine hypersonic inlet flow fields
Document ID
19650043887
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Benson, J. L.
Maslowe, S. A.
Date Acquired
August 2, 2013
Publication Date
June 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 65-617
Report Number: AIAA PAPER 65-617
Accession Number
65A26591
Funding Number(s)
CONTRACT_GRANT: NAS2-1460
Distribution Limits
Public
Copyright
Other
Keywords
AIR BREATHING ENGINE
FLOW FIELD
INLET FLOW
BLUNT BODY
HYPERSONIC BOUNDARY LAYER

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