Wind Tunnel Test of Gurney Flaps and T-Strips on an NACA 23012 Wing-Reference-Cited by-同舟云学术

Wind Tunnel Test of Gurney Flaps and T-Strips on an NACA 23012 Wing

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Applied Aerodynamics Conference
language:
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Author:

Cavanaugh Michael¹,Robertson Paul²,Mason William¹

Affiliation:

1. Virginia Tech

2. Aeronautical Testing Service, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4175

Reference17 articles.

1. Study of an Open-Wheel Racing-Car's Rear-Wing Aerodynamics

2. 3Kentfield, J. A. C. "Theoretically and Experimentally Obtained Performances of Gurney-Flap Equipped Wind Turbines," WindEngineering,Vol.18,No.2,March1994,pp.63-74.

3. 4Bieniawski, S., Kroo, I. "Development and Testing of an Experimental Aeroelastic Model with Micro-Trailing Edge Effectors," AIAA 2003-220,January2003.

4. 5Thiel, M. R., Lesieutre, G. A., Maughmer, M. D., Koopmann, G. H. "Actuation of an Active Gurney Flap for Rotorcraft Application,"AIAA 2006-2181,May 2006.

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