Controlled leading-edge suction for management of unsteady separation over pitching airfoils-Reference-Cited by-同舟云学术

Controlled leading-edge suction for management of unsteady separation over pitching airfoils

Published:1996-11 Issue:11 Volume:34 Page:2327-2336
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Alrefai Mah'd¹,Acharya Mukund¹

Affiliation:

1. Illinois Institute of Technology, Chicago, Illinois 60616

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.13398

Reference8 articles.

1. Metwally, M. H. "Investigation and Control of the UnsteadyFlow over a Pitching Airfoil," Ph.D. Thesis,Mechanical and Aerospace Engineering Dept., Illinois Inst. of Technology, Chicago, IL,Dec. 1990.

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

3. 3Karim, M. A. "Experimental Investigation of the Formation and Control of the Dynamic-Stall Vortex over a Pitching Airfoil," M.S. Thesis,Mechanical and Aerospace Engineering Dept., Illinois Inst. of Technology,Chicago, IL,May 1992.

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

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