The effect of compressibility on suppression of dynamic stall using a slotted airfoil-Reference-Cited by-同舟云学术

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The effect of compressibility on suppression of dynamic stall using a slotted airfoil

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Carr L.¹,Chandrasekhara M.²,Wilder M.³,Noonan K.⁴

Affiliation:

1. U.S. Army, Aeroflightdynamics Directorate; NASA, Ames Research Center, Moffett Field, CA

2. Navy-NASA Joint Inst. of Aeronautics, Monterey, CA

3. MCAT, Inc., Mountain View, CA

4. U.S. Army, Aeroflightdynamics Directorate; NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-332

Reference23 articles.

1. Progress in analysis and prediction of dynamic stall

2. Compressibility effects on dynamic stall

3. The effect of a leading-edge slat on the dynamic stall of an oscillating airfoil

Cited by 7 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. Numerical Investigations of a Back-Flow Flap for Dynamic Stall Control;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2014

2. Dynamic Stall Control by Passive Disturbance Generators;AIAA Journal;2013-09

3. Dynamic Stall Control Using a Model-Based Observer;Journal of Aircraft;2003-03

4. Compressible Dynamic Stall Control: Comparison of Two Approaches;Journal of Aircraft;2001-05

5. Dynamic Stall Control by Periodic Excitation, Part 2: Mechanisms;Journal of Aircraft;2001-05

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