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Investigation of an underslung normal-wedge inlet at free-stream mach numbers from 1.50 to 1.99Wedge and scoop air inlet performance and thrust minus drag comparisons at free stream in supersonic wind tunnel test
Document ID
19650013683
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
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 19, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-E56F27
Report Number: NACA-RM-E56F27
Accession Number
65N23284
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC WIND TUNNEL
FREE STREAM
AIR INLET
THRUST MEASUREMENT
DRAG MEASUREMENT

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