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Investigation of high-angle-of-attack performance of a 14 deg ramp-type inlet in various circumferential body locations, Mach number range 1.5 to 2.0Internal flow performance of fixed 14 deg ramp inlet from zero to 20 deg angle of attack at supersonic free stream
Document ID
19660024049
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Chiccine, B. G. (NASA Lewis Research Center Cleveland, OH, United States)
Mitchell, G. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 26, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-E57C12A
Accession Number
66N33339
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC FLOW
ANGLE OF ATTACK
FREE STREAM
INLET FLOW

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