Effects of pulsed endwall air injection on corner separation and vortical flow of a compressor cascade
Author:
Affiliation:
1. School of Power and Energy, Northwestern Polytechnical University, Xi’an, People’s Republic of China
Funder
National Natural Science Foundation of China
National Science and Technology Major Project
Publisher
Informa UK Limited
Subject
Modeling and Simulation,General Computer Science
Link
https://www.tandfonline.com/doi/pdf/10.1080/19942060.2022.2046643
Reference37 articles.
1. Experimental Investigations on Highly Loaded Compressor Airfoils With Active Flow Control Under Non-Steady Flow Conditions in a 3D-Annular Low-Speed Cascade
2. Three-Dimensional Flow in a Highly Loaded Single-Stage Transonic Fan
3. Influence of Endwall Air Injection with Discrete Holes on Corner Separation of a Compressor Cascade
4. Control of separations in a highly loaded diffusion cascade by tailored boundary layer suction
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