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PERFORMANCE OF AN ALL-INTERNAL CONICAL COMPRESSION INLET WITH ANNULAR THROAT BLEED AT MACH NUMBER 5.0Internal compression inlet with throat bleed-off at hypersonic flow
Document ID
19630008168
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Obery, L. J. (NASA Lewis Research Center Cleveland, OH, United States)
Stitt, L. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
August 6, 1958
Subject Category
Aircraft
Report/Patent Number
NACA-RM-E58E14
Report Number: NACA-RM-E58E14
Accession Number
63N18045
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
INTERNAL COMPRESSION INLET
THROAT
BLEED-OFF

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