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Preliminary Transient Performance Data on the J73 Turbojet EngineA program was undertaken to determine the J73 turbojet engine compressor stall and surge characteristics and combustor blow-out limits enc ountered during transient engine operation. Data were obtained in the form of oscillograph traces showing the time history of several engi ne parameters with changes in engine fuel flow. The data presented in this report are for step and ramp changes in fuel flow at an altitude of 45,000 feet and flight Mach numbers of 0 and 0.8.
Document ID
20090026297
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
McAulay, John E. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Wallner, Lewis E. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
June 30, 1953
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-SE53F30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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