Partial Leading Edge Forcing of a Delta Wing at High Angles of Attack-Reference-Cited by-同舟云学术

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Partial Leading Edge Forcing of a Delta Wing at High Angles of Attack

Published:2002-06-24 Issue: Volume: Page:
ISSN:
Container-title:1st Flow Control Conference
language:
Short-container-title:

Author:

Siegel Stefan¹,McLaughlin Thomas¹,Albertson Julie¹

Affiliation:

1. U.S. Air Force Academy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-3268

Reference12 articles.

1. PIV measurements on a delta wing with periodic blowing and suction

2. Guy, Y., Morrow, J. A., McLaughlin, T. E. "Control of Vortex Breakdown on a Delta Wing by Periodic Blowingand Suction", AIAA Paper 99-0132,1999.

3. Greenblat, D. and Wygnanski, I. "Dynamic Stall Control by Oscillatory Forcing", AIAA Paper 98-0676,1998.

Cited by 4 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. Parametric Investigations of the Leading Edge Vortex on a Delta Wing;41st AIAA Fluid Dynamics Conference and Exhibit;2011-06-14

2. Delta Wing Flow Control Using Dielectric Barrier Discharge Actuators;25th AIAA Applied Aerodynamics Conference;2007-06-15

3. Unsteady aerodynamics of nonslender delta wings;Progress in Aerospace Sciences;2005-10

4. Active Flow Control of a Delta Wing at High Incidence Using Segmented Piezoelectric Actuators;1st Flow Control Conference;2002-06-24

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