Steady Performance Measurements of a Turbofan Engine With Inlet Distortions Containing Co- and Counterrotating Swirl From an Intake Diffuser for Hypersonic Flight

[+] Author and Article Information
Norbert R. Schmid, Dirk C. Leinhos, Leonhard Fottner

Institut für Strahlantriebe, Universität der Bundeswehr München, D-85577 Neubiberg, Germany

J. Turbomach 123(2), 379-385 (Feb 01, 2000) (7 pages) doi:10.1115/1.1343466 History: Received February 01, 2000
Copyright © 2001 by ASME
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Grahic Jump Location
Variation of the thrust vector
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Measured relative total pressure, cross velocities
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Measured distortion parameters (model)
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Distortion parameters delta wing simulator
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LARZAC 04 C5 test engine
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Positions of the low-frequency instrumentation
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Relative specific fuel consumption
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Position of the high frequency probes relative to the CO and COUNTER distortions
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(a) CO and (b) COUNTER pressure signals near stall




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