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RESEARCH PAPERS

Intra-Stator Transport of Rotor Wakes and Its Effect on Compressor Performance

[+] Author and Article Information
J. L. Kerrebrock

Massachusetts Institute of Technology; Pratt & Whitney Division, United Aircraft Corp.

A. A. Mikolajczak

Compressor Research Group, Pratt & Whitney Division, United Aircraft Corp., East Hartford, Conn.

J. Eng. Power 92(4), 359-368 (Oct 01, 1970) (10 pages) doi:10.1115/1.3445365 History: Received January 13, 1970; Online July 14, 2010

Abstract

The stagnation temperature profiles which have been observed recently downstream of the stators in high Mach number compressor stages are shown to be due to transport of the rotor wakes across the main streamlines during their passage through the stator. The rotor wake fluid has energy in excess of the inviscid flow, and it is collected by the pressure side of the stator. A wake transport theory is presented, which connects the temperature profile to the rotor blade loss factor, and so provides a new method for determination of the losses in a rotor under actual operating conditions. The theory compares favorably with a special helium-tracer experiment designed to check it, as well as with temperature measurements in two high Mach number stages.

Copyright © 1970 by ASME
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