Flow stability analysis on low-speed compressor with swept rotor blades under radial inlet distortions-Reference-Cited by-同舟云学术

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Flow stability analysis on low-speed compressor with swept rotor blades under radial inlet distortions

Published:2024-09 Issue: Volume:152 Page:109362
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sun Dakun,Zhu Hengyi^ORCID,Xu Dengke^ORCID,Ni Haoyu,Sun Xiaofeng

Publisher

Elsevier BV

Reference40 articles.

1. Compressor surge and stall propagation;Emmons;J. Fluids Eng.,1955

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

3. A theory of post-stall transients in axial compression systems: part II—application;Greitzer;J. Eng. Gas Turbine Power,1986

4. Computational study of rotating-stall inception in axial compressors;He;J. Propuls. Power,1997

5. Role of blade passage flow structures in axial compressor rotating stall inception;Hoying;J. Turbomach.,1999

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