An investigation of aerodynamic performance of aeroengine fan and booster under non-uniform inlet conditions-Reference-Cited by-同舟云学术

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An investigation of aerodynamic performance of aeroengine fan and booster under non-uniform inlet conditions

Published:2023-05-26 Issue: Volume: Page:
ISSN:2523-3947
Container-title:Aerospace Systems
language:en
Short-container-title:AS

Author:

Qiu Zetian,Zhu Zhongyu,Liu Xiaohua^ORCID

Funder

National Natural Science Foundation of China

the Open Research Subject of Key Laboratory (Fluid Machinery and Engineering Research Base) of Sichuan Province

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42401-023-00229-2.pdf

Reference31 articles.

1. Emmons HW, Pearson CE, Grant HP (1955) Compressor surge and stall propagation. Trans ASME 77:455–469

2. Greitzer EM (1976) Surge and rotating stall in axial flow compressors: part 1 and part 2. J Eng Power 98:190–217

3. Moore FK, Greitzer EM (1986) A theory of post-stall transients in axial compression systems: part I - development of equations. J Eng Gas Turbines Power 108:68–76

4. McDougall NM, Cumpsty NA, Hynes TP (1990) Stall precursors in axial compressors. J Turbomach 112:116–125

5. Garnier VH, Epstein AH, Greitzer EM (1991) Rotating waves as a stall precursors indication in axial compressors. J Turbomach 113:290–302

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