Aeroelastic wing with leading- and trailing-edge control surfaces

Journal of Aircraft

Volumn 40, Issue 3, 2003, Pages 559-565

  Dowell, Earl H ^a   Bliss, Donald B ^a   Clark, Robert L ^a  

^a Duke University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; FLIGHT DYNAMICS; LIFT; MATHEMATICAL MODELS; ROTATION; STIFFNESS; TORSION TESTING;

AEROELASTIC WING; CONTROL SURFACES;

WINGS;

EID: 0037529037     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.3130     Document Type: Article

References (18)

1. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L. Aeroelasticity, Addison Wesley Longman Reading, MA, 1955, pp. 460-474.
2. Dowell, E. H., Crawley, E. F., Curtiss, H. C., Jr., Peters, D. A., Scanlan, R. H., and Sisto, F., A Modern Course in Aeroelasticity, 3rd ed., Kluwer, Dordrecht, The Netherlands, 1995, pp. 25-41.
3. Noll, T. E., and Eastep, F. E., "Active Flexible Wing Program," Journal of Aircraft, Vol. 32, No. 1, 1995, p. 9.
4. Woods-Vedeler, J. A., Pototzky, A. S., and Hoadley, S. T., "Rolling Maneuver Load Alleviation Using Active Controls," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 68-76.
5. Andersen, G., Forster, E., Kolonay, R., and Eastep, F., "Multiple Control Surface Utilization in Active Aeroelastic Wing Technology," Journal of Aircraft, Vol. 34, No. 4, 1997, pp. 552-557.
6. Zink, P. S., Mavris, D. N., Love, M. H., and Karpel, M., "Robust Design for Aeroelastically Tailored/Active Aeroelastic Wing," AIAA Paper 98-4781, Sept. 1998.
7. Weisshaar, T. A., Duke, D. K., and Dobbins, A., "Active Aeroelastic Tailoring with Adaptive Continuous Control Surfaces," AIAA Paper 2000-1619, 2000.
8. Flick, P. M., and Love, M. H., "The Impact of Active Aeroelastic Wing Technology on Conceptual Aircraft Design," Research and Technology Organization Air Vehicle Technology Specialists Meeting on Structural Aspects of Flexible Aircraft Control, Paper RTO MP-36, Oct. 1999.
9. Yurkovich, R. R., "Optimum Wing Shape for an Active Flexible Wing," Proceedings of the AIAA/ASME/ASCE/ARS 36th Structures, Structural Dynamics, and Materials Conference, AIAA-95-1220, 1995.
10. Pendleton, E., Lee, M., and Wasserman, L., "Application of Active Flexible Wing Technology to the Agile Falcon," Journal of Aircraft, Vol. 29, No. 3, 1992, pp. 444-451.
11. Pendleton, E., Bessette, D., Field, P., Miller, G., and Griffin, K., "Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development," Journal of Aircraft, Vol. 37, No. 4, 2000, pp. 554-561.
12. Kuethe, A. M., and Chow, C.-Y., Foundations of Aerodynamics: Bases of Aerodynamic Design, Wiley, New York, 1986, pp. 151-153.
13. Dowell, E. H., and Hall, K. C., "Modeling of Fluid-Structure Interaction," Annual Review of Fluid Mechanics, Vol. 33, 2001, pp. 445-490.
14. Hancock, G. J., "The Static Aeroelastic Deformation of Slender Configurations. Part I: Some Elementory Concepts of Static Deformation," Slender Plate Aircraft, Including Nonlinear Aerodynamics," Aeronautical Quarterly, Vol. 65, Aug. 1961, pp. 293-308
15. Hancock, G. J., "The Static Deformation of Slender Configurations. Part II: Some Calculations on Slender Plate Aircraft, Including Nonlinear Aerodynamics," Aeronautical Quarterly, Vol. 65, Nov. 1961, pp. 372-394.
16. Prechtl, E. F., and Hall, S. R., "Design of a High Efficiency, Large Stroke, Electromechanical Actuator," Journal of Smart Materials and Structures, Vol. 8, No. 1, 1999, pp. 13-30.
17. Ardelean, E., and Clark, R. L., "V-stack Piezoelectric Actuator," Proceedings of the SPIE, Vol. 4333, Smart Structures and Materials, Society of Photo-Optical Instrumentation Engineers, Bellingham, WA, 2001, pp. 322-333.
18. Sahin, B., Akilli, H., Lin, J.-C., and Rockwell, D., "Vortex Breakdown-Edge Interaction: Consequence of Edge Oscillations," AIAA Journal, Vol. 39, No. 5, 2001, pp. 865-876.