Three-dimensional compressor blading design improvements in low-speed model testing

Author:

Zhang ChenkaiORCID,Hu Jun,Li Jun,Wang Zhiqiang

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. Loss reduction in axial-flow compressor through low-speed model testing;Wisler;J. Eng. Gas Turbines Power,1985

2. Core Compressor Exit Stage Study, Volume I – Blading Design;Wisler,1977

3. Improving Compressor and Turbine Performance Through Cost-Effective Low-Speed Testing;Wisler,1999

4. Low Speed Axial Compressor Design and Evaluation; High Speed Representation and Endwall Flow Control Studies;Lyes,1999

5. The use of sweep and dihedral in multistage axial flow compressor blading. Part I: University research and methods development;Gallimore;J. Turbomach.,2002

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