An Experimental Study of Rotating Stall in a Multistage Axial-Flow Compressor

[+] Author and Article Information
D. K. Das

Division of Engineering Technology, SUNY College of Technology, Utica, N.Y.

H. K. Jiang

Department of Jet Propulsion, Peking Institute of Aeronautics and Astronautics, Peking, People’s Republic of China

J. Eng. Gas Turbines Power 106(3), 542-551 (Jul 01, 1984) (10 pages) doi:10.1115/1.3239605 History: Received July 06, 1983; Online October 15, 2009


The flow field and the distribution of the flow parameters in the rotating stall regime in a three stage axial flow compressor were obtained in detail using three-hole cylindrical probes containing fast response transducers in association with a digital data acquisition system and an ensemble averaging technique. An appreciable amount of experimental data are presented in this paper with a critical discussion on those.

Copyright © 1984 by ASME
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