Experimental investigation of instability inception on a transonic compressor under various radial distributions of loading-Reference-Cited by-同舟云学术

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Experimental investigation of instability inception on a transonic compressor under various radial distributions of loading

Published:2023-03 Issue: Volume:134 Page:108167
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Pan Tianyu,Yan Zhaoqi,Yan Jiandong^ORCID,Sun Dakun,Li Qiushi

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

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

2. Review of tip air injection to improve stall margin in axial compressors;Li;Prog. Aerosp. Sci.,2019

3. Passive Endwall Treatments for Enhancing Stability;Hathaway,2007

4. A study of spike and modal stall phenomena in a low-speed axial compressor;Camp;ASME J. Turbomach.,1998

5. Numerical and experimental study for short wavelength stall inception in a low-speed axial compressor;Hah,1999

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1. Experimental investigation of instability inception on a transonic compressor under various inlet guide vanes;Chinese Journal of Aeronautics;2024-09

2. A numerical simulation strategy for a compressor’s underlying axisymmetric characteristic and its application in body force model;Chinese Journal of Aeronautics;2024-08

3. Effects of Re on blade load temporal-spatial distribution and correlation with flow stability of transonic compressor under inlet distortion;Aerospace Science and Technology;2024-04

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