Active Flow-Separation Control on a High-Lift Wing-Body Configuration-Reference-Cited by-同舟云学术

Active Flow-Separation Control on a High-Lift Wing-Body Configuration

Published:2013-01 Issue:1 Volume:50 Page:56-72
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Ciobaca Vlad¹,Kühn Timo¹,Rudnik Ralf¹,Bauer Matthias²,Gölling Burkhard³,Breitenstein Wiebke⁴

Affiliation:

1. Head of Transport Aircraft Department, DLR, German Aerospace Center, 38108 Braunschweig, Germany

2. Department of Astronautics and Aeronautics, Technical University Berlin, 10587 Berlin, Germany

3. Airbus Operations GmbH, 28199 Bremen, Germany

4. University of Applied Sciences Emden/Leer, 26723 Emden, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031659

Reference35 articles.

1. Flow Control

2. The control of flow separation by periodic excitation

3. McLeanJ. D.CrouchJ. D.StonerR. C.SakuraiS.SeidelG. E.FeifelW. M.RushH. M. “Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft,” NASA CR 209338, 1999.

4. RudolphP. K. C. “High-Lift Systems on Commercial Subsonic Airliners,” NASA CR 4746, Sept. 1996.

5. Improving Flap Aerodynamics Using Oscillatory Jet Control

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