A Novel Airfoil Circulation Augment Flow Control Method Using Co-Flow Jet-Reference-Cited by-同舟云学术

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A Novel Airfoil Circulation Augment Flow Control Method Using Co-Flow Jet

Published:2004-06-20 Issue: Volume: Page:
ISSN:
Container-title:2nd AIAA Flow Control Conference
language:
Short-container-title:

Author:

Zha Ge-Cheng¹,Paxton Craig¹

Affiliation:

1. University of Miami

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2208

Reference26 articles.

1. Flow Control: The Future

2. Frontiers of Flow Control

3. L. C. Bradley, “An Experimental Investigation of A Sting-Mounted Finite Circulation Control Wing.” M.S. Thesis,Air Force Institute of Technology, 1995.

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