Bi-global stability analysis on flow separation of two-dimensional compressor cascade-Reference-Cited by-同舟云学术

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Bi-global stability analysis on flow separation of two-dimensional compressor cascade

Published:2023-11 Issue: Volume:142 Page:108591
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sun Dakun,Ni Haoyu,Fang Yibo,Xu Dengke^ORCID,Sun Xiaofeng

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference38 articles.

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

2. Rotating Waves as a Stall Inception Indication in Axial Compressors;Garnier,1991

3. Direct numerical simulation of turbulence in a nominally zero-pressure-gradient flat-plate boundary layer;Wu;J. Fluid Mech.,2009

4. Review of rotating wing dynamic stall: experiments and flow control;Gardner;Prog. Aerosp. Sci.,2023

5. Influence of surface flow on aerodynamic loads of a cantilever wing;Huang;AIAA J.,1996

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