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Investigation of an Underslung Scoop Inlet at Mach Numbers to 1.99Supersonic wind tunnel test of underslung scoop inlet on body of revolution
Document ID
19650018860
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Mc Kevitt, F. (NASA Lewis Research Center Cleveland, OH, United States)
Vargo, D. J. (NASA Lewis Research Center Cleveland, OH, United States)
Weinstein, M. I. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 13, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-E56L11
Accession Number
65N28461
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BODY OF REVOLUTION
SUPERSONIC WIND TUNNEL
AIR INLET

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