Post-stall flow control on an airfoil by local unsteady forcing. I - Lift, drag, and pressure characteristics-Reference-Cited by-同舟云学术

Post-stall flow control on an airfoil by local unsteady forcing. I - Lift, drag, and pressure characteristics

Published:1997-06-29 Issue: Volume: Page:
ISSN:
Container-title:4th Shear Flow Control Conference
language:
Short-container-title:

Author:

Wu Jain-Ming¹,Lu Xi-Yun¹,Denny Andrew¹,Fan Meng¹,Wu Jie-Zhi¹,Wu Jain-Ming¹,Lu Xi-Yun¹,Denny Andrew¹,Fan Meng¹,Wu Jie-Zhi¹

Affiliation:

1. Tennessee, Univ., Tullahoma

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2063

Reference36 articles.

1. Influence of Sound upon Separated Flow over Wings

2. Wu, J.Z., Vakili, A.D., and Wu, J.M. 1991.Review of the physics of enhancing vortex lift by unsteady excitation. Prog. Aerospace Sci. 28, ed. by A.D. Young, Pergamon Press, 73-131.

3. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation

4. On the flow of air behind an inclined flat plate of infinite span

5. Critzos, C.C., Heyson, H.H., and Boswinkle, R.W. 1955. Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 360°. NACA TN 3361.

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