Flow separation control using unsteady pulsed suction through endwall bleeding holes in a highly loaded compressor cascade-Reference-Cited by-同舟云学术

Flow separation control using unsteady pulsed suction through endwall bleeding holes in a highly loaded compressor cascade

Published:2018-01 Issue: Volume:72 Page:455-464
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Hongxin,Chen Shaowen,Meng Qinghe,Wang Songtao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

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4. Development of design methodology for a synthetic jet actuator array for flow separation control applications;Jabbal;Proc. Inst. Mech. Eng., G J. Aerosp. Eng.,2013

5. Comparative study of boundary layer control around an ordinary airfoil and a high lift airfoil with secondary blowing;James;Comput. Fluids,2017

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