Hysteresis behaviors of compressor rotating stall with cusp catastrophic model-Reference-Cited by-同舟云学术

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Hysteresis behaviors of compressor rotating stall with cusp catastrophic model

Published:2018-05 Issue:5 Volume:31 Page:1075-1084
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LI Zhiping,ZHANG Peng,PAN Tianyu,LI Qiushi,ZHANG Jian

Funder

National Natural Science Foundation of China

Aeronautics Power Foundation of China

China Postdoctoral Science Foundation

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference29 articles.

1. Surge and rotating stall in axial flow compressors–Part I: Theoretical compression system model;Greitzer;J Eng Power,1976

2. Surge and rotating stall in axial flow compressors–Part II: Experimental results and comparison with theory;Greitzer;J Eng Power,1976

3. Stall inception in axial flow compressor;Day;J Turbomach,1993

4. Rotating waves as a stall indication in axial compressors;Garnier;J Turbomach,1991

5. Effect of blade tip winglet on the performance of a highly loaded transonic compressor rotor;Han;Chin J Aeronaut,2016

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