Control of vortex breakdown on a delta wing by periodic blowing and suction-Reference-Cited by-同舟云学术

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Control of vortex breakdown on a delta wing by periodic blowing and suction

Published:1999-01-11 Issue: Volume: Page:
ISSN:
Container-title:37th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Guy Yair¹,Morrow Julie¹,McLaughlin Thomas¹

Affiliation:

1. U.S. Air Force Academy, Colorado Springs, CO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-132

Reference14 articles.

1. Greenblat, D. and Wygnanski, I. "Dynamic Stall Control, by Oscillatory Forcing", ALL4 Paper 98-0676,1998.

2. Nishri, B. "On the Dominant Mechanisms Governing Active Control of Separation", Ph.D. Thesis,Tel-Aviv University, Israel

3. Nishri, B. and Wygnanski, I. "eonthe Flow Separation and its Control", Computational Methods in Applied Science,1996.

4. Delay of airfoil stall by periodic excitation

5. Nave, T. "The Effect of Sweep on Separation Control over anAirfoil", M.Sc. Thesis,Tel-Aviv University, Israel, 1997.

Cited by 14 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. Manipulation of Leading-Edge Vortex Flow;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2020-10-18

2. Control of Flow Structure over a Nonslender Delta Wing Using Periodic Blowing;AIAA Journal;2018-01

3. Effects of Synthetic Jet Actuator (SJA) on Flow Topology of Blunt-Edged UTM VFE2 Wing Model;55th AIAA Aerospace Sciences Meeting;2017-01-05

4. Plasma control of vortex flow on a delta wing at high angles of attack;Experiments in Fluids;2013-08

5. Controlled Vortex Breakdown on Modified Delta Wings;Journal of Visualization;2007-09

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