Study of Shock Wave Control by Suction & Blowing on a Highly-loaded Transonic Compressor Cascade
Author:
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2013-0005/pdf
Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Variations of the shock and secondary flow structure in a transonic compressor cascade with outlet back pressure;Physics of Fluids;2024-06-01
2. Effects of Number of Bleed Holes on Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator;Journal of Thermal Science;2024-01-10
3. Experimental and Numerical Investigations of Shock-Wave Boundary Layer Interactions in a Highly Loaded Transonic Compressor Cascade;Journal of Thermal Science;2023-12-06
4. Effect of combined boundary layer suction on the separation control in a highly loaded transonic compressor cascade;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2023-10-03
5. Study of flow separation control by bleed slot and bleed holes in a transonic compressor cascade;Physics of Fluids;2023-09-01
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