Three-dimensional optimization of squealer-tip for a transonic axial-flow compressor rotor blade

Author:

Heidarian Shahri Mojtaba,Habibzadeh Saeid,Madadi AliORCID

Publisher

Elsevier BV

Subject

Multidisciplinary

Reference16 articles.

1. Effect of rotor tip winglet on the performance and stabilityof a transonic axial compressor;Shivaramaiah,2017

2. Zeng F., DU J., Huang L., Xuan L., Zhao Q., Zou Z., An experimental method for squealer tip flow field considering relative casing motion, Chin. J. Aeronaut. (2020)Volume: 33, Issue: 7, Page Range: 1942-1952.

3. Effects of suction side squealer tip on the performance of a low-speed axial compressor;Zhang;J. Therm. Sci.,2012

4. Experimental investigation of effects of suction-side squealer tip geometry on the flow field in a larg-scale axial compressor using SPIV;Hongwei;Journal of Termal Science,2015

5. Shaobing H., Jingjun Z., Effect of blade tip winglet on the performance of a highly loaded transonic compressor rotor, Chin. J. Aeronaut. (2016)Volume: 29, Issue: 3, Page Range: 653-661.

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