Impact of non-axisymmetric tip clearance on the aerodynamic and aeroelastic stabilities of a transonic compressor

Author:

Xia Kailong,Chen Huayin,Deng HefangORCID,Zhu Mingmin,Qiang Xiaoqing,Teng JinfangORCID

Publisher

Elsevier BV

Reference49 articles.

1. Stall, surge, and 75 years of research;Day;J. Turbomach.,2016

2. Graf M.B., Wong T.S., Greitzer E.M., et al. Effects of Non-Axisymmetric Tip Clearance On Axial Compressor Performance and Stabilityc//Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 1997, 78682: V001T03A066.

3. Nonuniform flow in a compressor due to asymmetric tip clearance;Song;J. Turbomach.,2000

4. Chen Y., Hou A., Zhang M., et al. Effects of Nonuniform Tip Clearance On Fan Performance and Flow Fieldc//Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2015, 56635: V02AT37A010.

5. Performance estimation method for non-uniform tip clearance cases;Chen;J. Propul. Power,2018

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