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PERFORMANCE OF VARIABLE TWO-DIMENSIONAL INLET DESIGNED FOR ENGINE-INLET MATCHING. I - PERFORMANCE AT DESIGN MACH NUMBER OF 3.07Supersonic performance of variable two-dimensional inlets designed for engine-inlet matching
Document ID
19630002647
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Beheim, M. A. (NASA Lewis Research Center Cleveland, OH, United States)
Gertsma, L. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
November 20, 1956
Subject Category
Aircraft
Report/Patent Number
NACA-RM-E56H23
Accession Number
63N12523
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ENGINE
TWO-DIMENSIONAL BODY
SUPERSONIC INLET
VARIABLE GEOMETRY STRUCTURE

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