Investigation of Aeroelastic Effects of a Circulation Controlled Wing
Author:
Affiliation:
1. Technische Universität Braunschweig, Braunschweig, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033780
Reference22 articles.
1. SFB 880: fundamentals of high lift for future commercial aircraft
2. Design and Analysis of a Droop Nose for Coanda Flap Applications
3. LighthillM. “Notes on the Deflection of Jets by Insertion of Curved Surfaces, and on the Design of Bends in Wind Tunnels,” Reports and Memoranda 2105, Aeronautical Research Council, London, 1945.
4. Aerodynamics of Powered High-Lift Systems
5. Development of advanced circulation control wing high-lift airfoils
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