Vortical Interactions Behind Deployable Vortex Generator for Airfoil Static Stall Control-Reference-Cited by-同舟云学术

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Vortical Interactions Behind Deployable Vortex Generator for Airfoil Static Stall Control

Published:2013-01 Issue:1 Volume:51 Page:240-252
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Joubert G.¹,Le Pape A.¹,Heine B.²,Huberson S.³

Affiliation:

1. Applied Aerodynamics Department, ONERA—The French Aerospace Lab, 92190 Meudon, France

2. Helicopters Department, German Aerospace Center (DLR), 37073 Göttingen, Germany

3. PRIME Institute, CNRS—Université de Poitiers–ENSMA, 86962 Futuroscope Chasseneuil, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J051767

Reference29 articles.

1. Fatigue Strength Improvements in Ti-6Al-4V Forgings

2. McAlisterK. W.TungC. “Suppression of Dynamic Stall with a Leading-Edge Slat on a VR-7 Airfoil,” NASA TR-TP-3357, 1993.

3. Unsteady Stall Control Using Dynamically Deforming Airfoils

4. Dynamic Stall Control by Leading Edge Vortex Generators

5. Passive Control of Compressible Dynamic Stall

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