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COMBUSTION PERFORMANCE OF TWO EXPERIMENTAL TURBOJET ANNULAR COMBUSTORS AT CONDITIONS SIMULATING HIGH-ALTITUDE SUPERSONIC FLIGHTPerformance of experimental annular turbojet combustors at simulated high altitude supersonic flight conditions
Document ID
19630003987
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Mark, H. (NASA Lewis Research Center Cleveland, OH, United States)
Norgren, C. T. (NASA Lewis Research Center Cleveland, OH, United States)
Zettle, E. V. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
March 26, 1954
Subject Category
Physics, Solid-State
Report/Patent Number
NACA-RM-E54A15
Report Number: NACA-RM-E54A15
Accession Number
63N13863
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMBUSTOR
HIGH ALTITUDE
COMBUSTION EFFICIENCY
TURBOJET ENGINE
SIMULATED ALTITUDE
SUPERSONIC SPEED
FLIGHT SIMULATION

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