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Research article

First published 2018-9

Active flow control by means of endwall synthetic jet on a high-speed compressor stator cascade

Yong Qin, Yanping Song, Fu Chen [...]

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2013-9

Vortex development induced by part gap geometry and endwall configurations for variable stator vanes in a compressor cascade

M Gottschall, K Vogeler

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2018-9

Flow separation control on a highly loaded compressor cascade using endwall synthetic jets

Yong Qin, Yanping Song, Ruoyu Wang [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2023-2

Corner separation control in compressor stators with jets from the blade leading edge

Huan Zheng, Zhenggui Zhou

Advances in Mechanical Engineering

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Research article

First published 2007-2

Innovative procedure to minimize multi-row compressor blade dynamic loading using rotor-stator interaction optimization

E Benini, A Toffolo

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2022-8

Effect of three non-axisymmetric stator schemes on compressor performance with distorted inlet

Wenguang Fu, Peng Sun

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2011-11

Experimental and numerical results of active flow control on a highly loaded stator cascade

M Hecklau, C Gmelin, W Nitsche [...]

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2021

Applications of little blades in a high-load compressor cascade with leaned blade

Shan Ma, Xiaolin Sun

Proceedings of the Institution of Mechanical Engineers,Part C: Journal of Mechanical Engineering Science

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Research article

First published 2021-2

Investigation on the aerodynamic performance of high camber turning angle cascade with tubercle leading edge

Baofeng Tu, Hao Wang, Jun Hu

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2014-6

The effect of different clearance geometry configurations on aerodynamic performance in a high-load compressor cascade

Shaowen Chen, Shijun Sun, Yunhe Lan [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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