Flow instability suppression and deep surge delay by non-axisymmetric vaned diffuser in a centrifugal compressor-Reference-Cited by-同舟云学术

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Flow instability suppression and deep surge delay by non-axisymmetric vaned diffuser in a centrifugal compressor

Published:2019-12 Issue: Volume:95 Page:105494
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sun Zhenzhong,Zheng Xinqian,Tamaki Hideaki,Kaneko Yuta

Funder

National Science and Technology Major Project

National Natural Science Foundation of China

Tsinghua University

IHI Corporation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. A new method for reliable performance prediction of multi-stage industrial centrifugal compressors based on stage stacking technique: part II–new integrated model verification;Al-Busaidi;Appl. Therm. Eng.,2015

2. Surge and rotating stall in axial flow compressors—part I: theoretical compression system model;Greitzer;J. Eng. Gas Turbines Power,1976

3. Experimental investigation of surge and stall in a high-speed centrifugal compressor;Zheng;J. Propuls. Power,2015

4. Compressor Aerodynamics;Cumpsty,2004

5. Compression system stability and active control;Paduano;Annu. Rev. Fluid Mech.,2001

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