Influence of SPS casing treatment on axial flow compressor subjected to radial pressure distortion-Reference-Cited by-同舟云学术

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Influence of SPS casing treatment on axial flow compressor subjected to radial pressure distortion

Published:2017-04 Issue:2 Volume:30 Page:685-697
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Li Fanyu,Li Jun,Dong Xu,Sun Dakun,Sun Xiaofeng

Funder

National Natural Science Foundation of China

National Basic Research Program of China

Aeronautical Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference35 articles.

1. Attenuation of circumferential inlet distortion in multistage axial compressors;Plourde;J Aircraft,1968

2. Cook R. Design and test of a highly-loaded three-stage, axial-flow compressor. Reston: AIAA; 1976. Report No.: AIAA 1976–6.

3. Tamaki T, Nagano S. Effects of inlet distortions on a multi-stage compressor. Reston: AIAA; 1979. Report No.: AIAA 1979–7003.

4. Performance of rotating cascades under the inlet-distortions: 1st report, performance under the radial distortions;Maekawa;Bull JSME,1979

5. Performance of rotating cascades under the inlet-distortions: 2nd report, performance under the circumferential distortions;Seo;Bull JSME,1981

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