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Performance of Twin-duct Variable-geometry Side Inlets at Mach Numbers of 1.5 to 2.0Supersonic wind tunnel test of twin-duct variable geometry side inlets
Document ID
19650018861
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Beheim, M. A. (NASA Lewis Research Center Cleveland, OH, United States)
Klann, J. L. (NASA Lewis Research Center Cleveland, OH, United States)
Yeager, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 21, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-E56K15
Accession Number
65N28462
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VARIABLE GEOMETRY STRUCTURE
SUPERSONIC WIND TUNNEL
AIR DUCT

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