Stability improvement without efficiency penalty of a transonic centrifugal compressor by casing treatment and impeller/diffuser coupling optimization-Reference-Cited by-同舟云学术

Stability improvement without efficiency penalty of a transonic centrifugal compressor by casing treatment and impeller/diffuser coupling optimization

Published:2022-08 Issue: Volume:127 Page:107685
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Xiaojian,Liu Zhengxian,Zhao Ming,Zhao Yijia,He Ying

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Performance enhancement of a centrifugal compressor stage using profiled end wall (PEW) treatments in the radial vaned diffuser;Lang;Aerosp. Sci. Technol.,2021

2. Stall, surge, and 75 years of research;Day;J. Turbomach.,2016

3. Two stall stages in a centrifugal compressor with a vaneless diffuser;Zhang;Aerosp. Sci. Technol.,2021

4. Combined flow control with full-span slot and end-wall boundary layer suction in a large-camber compressor cascade;Wang;Aerosp. Sci. Technol.,2021

5. Casing treatment and inlet swirl of centrifugal compressors;Chen;J. Turbomach.,2013

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