Investigation of the controlling mechanisms of blade slotting technology on the shock-wave-induced corner separation-Reference-Cited by-同舟云学术

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Investigation of the controlling mechanisms of blade slotting technology on the shock-wave-induced corner separation

Published:2023-09 Issue: Volume:140 Page:108491
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Hejian,Liu Bo,Mao Xiaochen,Zhang Botao^ORCID,Yang Zonghao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference54 articles.

1. Development of fan/compressor techniques and suggestions on further researches;Chen;J. Aerosp. Power,2002

2. The development trends and prospect of world aeropropulsion technology in the 21st century;Liu;Eng. Sci.,2004

3. Historic opportunities of aeropropulsion development;Liu;Aeroengine,2005

4. Experimental investigation of the three-dimensional flow in an annular compressor cascade;Schulz;J. Turbomach.,1988

5. Three Dimensional Flow in a Linear Compressor Cascade at Design Conditions;Kang,1991

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation of control effects of end-wall self-adaptive jet on three-dimensional corner separation of a highly loaded compressor cascade;Chinese Journal of Aeronautics;2024-06

2. Proof of concept study on a self-driven pulsed jet on a compressor stator blade by numerical simulation;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-11-27

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