Flutter suppression using Micro-Trailing Edge Effectors

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  Bieniawski, Stefan ^a   Kroo, Ilan M ^a  

^a Department of Aeronautics and Astronautics Department of Mechanical Engineering and Industrial for Computational and Mathematical Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC CONTROL; ANALYTICAL PREDICTIONS; CLOSED-LOOP TESTING; EXPERIMENTAL MODELING; FLOW CONTROL DEVICES; FLUTTER SUPPRESSION; HIGH-ASPECT RATIO WING; REINFORCEMENT LEARNING TECHNIQUES;

ASPECT RATIO; CONTROL; CONTROLLERS; REINFORCEMENT LEARNING; STRUCTURAL DYNAMICS;

FLUTTER (AERODYNAMICS);

EID: 84896693884     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Nae, C., "Synthetic Jet Influence on NACA 0012 Airfoil at High Angles of Attack, " AIAA Paper 98-4523.
2. Seifert, A., Darabi, A., Wygnanski, I., "Delay of Airfoil Stall by Periodic Excitation, " Journal of Aircraft, Vol. 32, No. 4, July-August 1996.
3. Kroo, I., Eaton, J., Prinz, F., "UAV Aeroelastic Control Using Redundant Microflaps, " Air Force Office of Scientific Research Program Review for Year I, 1999.
4. Solovitz, S., Eaton, J.K., "Aeroelastic Control Using Redundant Microactuators, " 3rd ASME/JSME Joint Fluids Engineering Conference, July 18-23, 1999, San Francisco, CA.
5. Kroo, I., Bieniawski, S., "UAV Aeroelastic Control Using Redundant Micro-Actuators, " Air Force Office of Scientific Research Program in Turbulence and Rotating Flows 2001 Contractor's Meeting, August 13-14, 2001, Seattle, WA.
6. Liebeck, R. H., "Design of Subsonic Airfoils for High Lift, " Journal of Aircraft, Vol. 15, No. 9, Sept., 1978.
7. Jeffrey, D., Zhang, X., and Hurst, D.W., "Aerodynamics of Gurney Flaps on a Single-Element High-Lift Wing, " Journal of Aircraft, Vol. 37, No. 2, 2000, pp. 295-301.
8. Storms, B. L, and Jang, C. S., "Lift Enhancement of an Airfoil Using a Gurney Flap and Vortex Generators, " Journal of Aircraft, Vol. 31, No. 3, June 1994.
9. Jang, C.S., Ross, J. C., and Cummings, R. M., "Computational Evaluation of an Airfoil with a Gurney Flap", AIAA Paper 92-2708, June 1992.
10. Kroo, I, "Aerodynamic Concepts for Future Aircraft, " 30th AIAA Fluid Dynamics Conference (AIAA 99-3524), Norfolk, Va, June-July 1999.
11. Lee, H., Kroo, I., Bieniawski, S., "Flutter Suppression for High Aspect Ratio Flexible Wings Using Microflaps, " AIAA 2002-1717, April 2002.
12. Jensen, D. W., Crawley, E.F., Dugundji, J., "Vibration of Cantilevered Graphite/Epoxy Plates with Bending-Torsion Coupling, " Journal of Reinforced Plastics and Composites, Vol. 1, July 1982, pp. 254-269.
13. Hollowell, S.J., and Dugundji, J., "Aeroelastic Flutter and Divergence of Stiffness Coupled, Graphite/Epoxy Cantilevered Plates, " Journal of Aircraft, Vol. 21, Jan 1984, pp 69-76.
14. Landsberger, B., and Dugundji, J., "Experimental Aeroelastic Behavior of Unswept and Forward Swept Graphite/Epoxy Wings, " Journal of Aircraft, Vol. 22, Aug 1985, pp 679-686.
15. Theodorsen, T., "General Theory of Aerodynamic Instability and the Mechanism of Flutter, " NACA TR 496, 1935.
16. Bryson, A, Control of Spacecraft and Aircraft, Princeton University Press, Princeton, New Jersey, 1994.
17. Richard Sutton and Andrew Barto, Reinforcement Learning: An introduction. MIT Press, 1998
18. Ng, Andrew Y., and Jordon, Michael, "PEGASUS: A policy search method for large MDPs and POMDPs. " In Uncertainty in Artificial Intelligence, Proceedings of the Sixteenth Conference, 2000.
19. Schneider, J.G., and Bagnell, J.A., "Autonomous Helicopter Control Using Reinforcement Learning Policy Search Methods, " Proceedings of the International Conference on Robotics and Automation, May 2000