Effect of bent inlet pipe on the flow instability behavior of centrifugal compressors-Reference-Cited by-同舟云学术

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Effect of bent inlet pipe on the flow instability behavior of centrifugal compressors

Published:2020-08 Issue:8 Volume:33 Page:2099-2109
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

SUN Zhenzhong,WANG Baotong,ZHENG Xinqian,KAWAKUBO Tomoki,TAMAKI Hideaki,NUMAKURA Ryuusuke

Funder

Tsinghua University

National Science and Technology Major Project

National Natural Science Foundation of China

IHI Corporation

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference28 articles.

1. Effect of internal heat leakage on the performance of a high pressure ratio centrifugal compressor;Moosania;Appl Therm Eng,2017

2. Mechanism of stall and surge in a centrifugal compressor with a variable vaned diffuser;Xue;Chin J Aeronaut,2018

3. Roles and mechanisms of casing treatment on different scales of flow instability in high pressure ratio centrifugal compressors;He;Aerosp Sci Technol,2019

4. Recent development of casing treatments for aero-engine compressors;Sun;Chin J Aeronaut,2019

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

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