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INVESTIGATION OF ADJUSTABLE SUPERSONIC INLET IN COMBINATION WITH J34 ENGINE UP TO MACH 2.0Pressure recovery in adjustable supersonic inlet combined with j34 turbojet engine up to mach 2.0
Document ID
19630004111
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Leissler, L. A. (NASA Lewis Research Center Cleveland, OH, United States)
Nettles, J. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
October 15, 1954
Subject Category
Propellants
Report/Patent Number
NACA-RM-E54H11
Report Number: NACA-RM-E54H11
Accession Number
63N13987
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC INLET
J-34 ENGINE
TURBOJET ENGINE
PRESSURE RECOVERY

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