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PERFORMANCE OF A SUPERSONIC RAMP-TYPE SIDE INLET WITH RAM-SCOOP THROAT BLEED AND VARYING FUSELAGE BOUNDARY-LAYER REMOVAL MACH NUMBER RANGE 1.5 TO 2.0Performance of supersonic ramp-type side inlet with ram-scoop throat bleed and varying fuselage boundary layer removal at low supersonic speeds
Document ID
19630002646
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Campbell, R. C. (NASA Lewis Research Center Cleveland, OH, United States)
Mitchell, G. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
January 17, 1957
Subject Category
Aircraft
Report/Patent Number
NACA-RM-E56I26
Report Number: NACA-RM-E56I26
Accession Number
63N12522
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THROAT
RAMP
SUPERSONIC INLET
FUSELAGE
BOUNDARY LAYER CONTROL
BLEED-OFF

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