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Research article

First published 2019-7

Variable nozzle turbocharger turbine performance improvement and shock wave alternation by distributing nozzle endwall clearances

Ben Zhao, Mingxu Qi, Harold Sun [...]

Proceedings of the Institution of Mechanical Engineers,Part D: Journal of Automobile Engineering

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Research article

First published 2022-5

Rotating tip clearance asymmetry and role of endwall injection in stability desensitization of a transonic fan

Hossein Khaleghi

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

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Research article

First published 2006-12

An investigation of the flowfield through a variable geometry turbine stator with vane endwall clearance

S. W T. Spence, J. W. O'Neill, G Cunningham

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

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Research article

First published 2023-6

Experimental study on the aerodynamic performance of variable geometry low-pressure turbine adjustable guide vanes

Yunjia Yao, Fengchao Li, Jiacheng Xiang [...]

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

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Research article

First published 2021-9

Effect of endwall suction on aerodynamic performance of compressor cascade with tip clearance at a large incidence angle

Botao Zhang, Bo Liu, Hejian Wang [...]

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

Open access

Research article

First published 2015

Understanding of the Interaction between Clearance Leakage Flow and Main Passage Flow in a VGT Turbine

Ben Zhao, Ce Yang, Liangjun Hu [...]

Advances in Mechanical Engineering

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Research article

First published 2017-11

Experiment study of the winglet-cavity tip on the aerodynamic performance in a turbine cascade

Shaowen Chen, Zhihua Zhou, Qinghe Meng [...]

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

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Research article

First published 2019-4

Experimental study on axially non-uniform clearances in a linear turbine cascade with a cavity squealer tip

Shaowen Chen, Qinghe Meng, Weihang Li [...]

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

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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 2021-9

Analysis of the relationship between turbulence characteristics and loss mechanism in the tip leakage flow of turbine blade

Hui Li, Xinrong Su, Xin Yuan

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

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