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Effect of hysteresis in axial compressors of gas-turbine engines

    Mykola Kulyk Affiliation
    ; Ivan Lastivka Affiliation
    ; Yuri Tereshchenko Affiliation
DOI: https://doi.org/10.3846/16487788.2012.753679

Abstract

The phenomenon of separated flow hysteresis in the process of the streamlining the axial compressor of gas-turbine engines is considered. Generalised results of research on the occurrence of hysteresis in the aerodynamic performance of compressor grids and its influence on the performance of the bladed disks of compressors that operate in real conditions of periodic circular non-uniformity are demonstrated.


First published online: 24 Dec 2012

Keyword : gas-turbine engines, axial compressor, hysteresis

How to Cite
Kulyk, M., Lastivka, I., & Tereshchenko, Y. (2012). Effect of hysteresis in axial compressors of gas-turbine engines. Aviation, 16(4), 97-102. https://doi.org/10.3846/16487788.2012.753679
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Dec 24, 2012
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