Application of Co-Flow Jet Concept on Thin Airfoil at High Angle of Attack-Reference-Cited by-同舟云学术

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Application of Co-Flow Jet Concept on Thin Airfoil at High Angle of Attack

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:3rd AIAA Flow Control Conference
language:
Short-container-title:

Author:

Rachman Arief¹,Tsai Her-Mann¹,Zha Ge-Cheng²

Affiliation:

1. National University of Singapore

2. University of Miami

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2849

Reference14 articles.

1. Aerodynamics for Revolutionary Air Vehicles

2. 3Sellars,N.D.,Wood,N.J,andKennaugh,A."DeltaWingCirculationControlUsingtheCoandaEffect,"AIAA2002-3269, AIAA1stFlowControlConference,StLouis,MO,June24-26,2002.

3. A Wind Tunnel Model to Explore Unsteady Circulation Control for General Aviation Applications

Cited by 1 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. Control of Flow Separation in S-Ducts via Flow Injection and Suction;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

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