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altitude wind tunnel investigation of xj34-we-32 engine performance without electronic controlAn investigation was conducted in the NACA Lewis altitude wind tunnel to evaluate the performance characteristics of an XJ34-WE-32 turbojet engine which was equipped with an afterburner, a variable-area exhaust nozzle, and an integrated electronic control. The data were obtained with the afterburner and electronic control inoperative. Performance data were obtained at altitudes from 5000 to 55,000 feet and flight Mach numbers from 0.28 to 1.06 for a complete range of operable engine speeds at each of four fixed positions of the variable-area exhaust nozzle.
Document ID
19930087885
Document Type
Other
Authors
Bloomer, Harry E
Walker, William J
Pantages, George L
Date Acquired
August 16, 2013
Publication Date
May 29, 1953
Report/Patent Number
NACA-RM-E51L12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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