Artificial neural networks for suppression of the dynamic-stall vortex over pitching airfoils-Reference-Cited by-同舟云学术

Artificial neural networks for suppression of the dynamic-stall vortex over pitching airfoils

Published:1996-01-15 Issue: Volume: Page:
ISSN:
Container-title:34th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Kawthar-Ali Mahmoud¹,Acharya Mukund¹

Affiliation:

1. Illinois Inst. of Technology, Chicago

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-540

Reference14 articles.

1. Unsteady pressure field and vorticity production over a pitching airfoil

2. Suppression of dynamic-stall vortices over pitching airfoils by leading-edge suction

3. Real-time prediction and control of three-dimensional unsteady separated flow fields using neural networks

4. 6Jacobson, S.A.,and Reynolds, W.C. "Active Control of Boundary Layer Wall Shear Stress Using Self-LearningNeural Networks,"AIAA PaperNo. 93-3273, January 1993.

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