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Performance of J33-A-27 Turbojet-Engine Compressor: Over - All Performance Characteristics of Modified Compressor at Equivalent Impeller Speeds from 6100 to 13,250 RPM - IIA modified J33-A-27 compressor was operated over a range of equivalent impeller speeds from 6100 to 13,250 rpm in order to obtain the over-all compressor performance. At the equivalent design speed of 11,800 rpm, the maximum efficiency of 0.764 and peak pressure ratio of 4.56 occurred at an equivalent weight flow of 104.07 pounds per second. At the highest equivalent speed (13,250 rpm) a maximum efficiency of 0.711, a maximum equivalent weight flow of 123.00 pounds per second, and a peak pressure ratio of 5.76 were obtained.
Document ID
20050019263
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Beede, William L.
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Ginsburg, Ambrose
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 22, 2013
Publication Date
January 1, 1950
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-SE50D25
Report Number: NACA-RM-SE50D25
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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