Use of Supersonic Microjets for Active Separation Control in Diffusers-Reference-Cited by-同舟云学术

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Use of Supersonic Microjets for Active Separation Control in Diffusers

Published:2003-06-23 Issue: Volume: Page:
ISSN:
Container-title:33rd AIAA Fluid Dynamics Conference and Exhibit
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Author:

Kumar Vikas¹,Alvi Farrukh¹

Affiliation:

1. FAMU/FSU College of Engineering

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4160

Reference22 articles.

1. Mayer, D.W., Anderson, B.H., Johnson T.A. "3D subsonic diffuser design and Analysis", AIAA98-3418.

2. Study of the compressible flow in a diffusing S-duct

3. Anabtawi,A.J., Blackwelder,R.F., Lissaman,P.B.S., Liebeck,R.H. "An experimental investigation of boundary layer ingestion in a diffusing S-duct with and withoutpassive flow control", AIAA 99-0739.

4. Rabe, D., Boles, A. And Russler, P. " Influence of Inlet distortion on transonic Compressor blade loading", AIAA 95-2461.

Cited by 3 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. A Theoretical Model for Microjet Separation Control;7th AIAA Flow Control Conference;2014-06-13

2. Use of High-Speed Microjets for Active Separation Control in Diffusers;AIAA Journal;2006-02

3. Efficient Control of Separation Using Microjets;35th AIAA Fluid Dynamics Conference and Exhibit;2005-06-06

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