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Analysis of Limitations Imposed on One-Spool Turbojet-Engine Designs by Turbines Having Downstream Stators at 0, 2.0, and 2.8 Flight Mach NumbersLimitations on turbojet engine design by turbines with downstream stators
Document ID
19630002631
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Cavicchi, R. H. (NASA Lewis Research Center Cleveland, OH, United States)
Constantine, A. B. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
January 19, 1955
Subject Category
Propellants
Report/Patent Number
NACA-RM-E54J14
Report Number: NACA-RM-E54J14
Accession Number
63N12507
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBINE
STATOR
TURBOJET ENGINE

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