Time-domain simulations of linear and nonlinear aeroelastic behavior

JVC/Journal of Vibration and Control

Volumn 6, Issue 8, 2000, Pages 1135-1175

  Preidikman, Sergio ^a,b   Mook, Dean ^a  

^a State University   (United States)

^b DEPARTAMENTO DE QUÍMICA   (Argentina)

Author keywords

Aeroelasticity; Flutter; Hopf bifurcation; Limit cycles; Motion on a torus

Indexed keywords

EID: 0034417611     PISSN: 10775463     EISSN: None     Source Type: Journal    
DOI: 10.1177/107754630000600802     Document Type: Article

References (24)

1. Atta, E. H., Kandil, O. A., Mook, D. T., and Nayfeh, A. H., 1976, "Unsteady flow over wings having sharp edge separations," in Proceedings of the Vortex Lattice Utilization Workshop, NASA SP-405, pp. 407-418.
2. Batchelor, G. K., 1967, An Introduction to Fluid Dynamics, Cambridge University Press, Cambridge, UK.
3. Belotserkovskii, S. M., 1955, "Horseshoe vorticies in nonsteady motion," Prikl. Mat. Mekh. 19(2), 159-164.
4. Belotserkovskii, S. M., 1968, "Calculation of the flow around wings of arbitrary planform over a wide range of angle of attack," Izv. Nauk SSSR, Mekh. Zhidk. Gaza 4, 32-44;
5. Fluid Dynamics 3(4), 20-27. Also NASA TT F-12 291, 1969.
6. Belotserkovskii, S. M. and Nisht, M. I., 1974, "Nonstationary nonlinear theory of a thin wing of arbitrary planform," Izv. Nauk SSSR, Mekh. Zhidk. Gaza 4, 100-108;
7. Fluid Dynamics 9(4), 583-589.
8. Bollay, W., 1939, "A non-linear theory and its application to rectangular wings of small aspect ratio," ZAMM 19(1), 21-35.
9. Carnahan, B., Luther, H. A., and Wilkes, J. O., 1969, Applied Numerical Methods, John Wiley, New York.
10. Fung, Y. C., 1969, An Introduction to the Theory of Aeroelasticity, Springer-Verlag, New York.
11. Hall, B. D., Mook, D. T., Nayfeh, A. H., and Preidikman, S., 2000, "A novel strategy for suppressing the flutter oscillations of aircraft wings," 38th Aerospace Sciences Meeting, Reno, NY January, AIAA Paper No. 2000-0904.
12. Kandil, O. A., Mook, D. T., and Nayfeh, A. H., 1976, "Nonlinear prediction of aerodynamic loads on lifting surfaces," Journal of Aircraft 13(1), 22-28.
13. Katz, J. and Plotkin, A., 1991, LOW-SPEED AERODYNAMICS From Wing Theory to Panel Methods, McGraw-Hill, New York.
14. Konstadinopoulos, P., Mook, D. T., and Nayfeh, A. H., 1985, "Subsonic wing rock of slender delta wings," Journal of Aircraft 22(3), 223-228.
15. Konstadinopoulos, P., Thrasher, D. F., Mook, D. T., Nayfeh, A. H., and Watson, L., 1985, "A vortex-lattice method for general, unsteady aerodynamics," Journal of Aircraft 22(1), 43-49.
16. Lee, B.H.K., Jiang, L. Y., and Wong, Y. S., 1999, "Flutter of an airfoil with a cubic restoring force," Journal of Fluids and Structures 13, 75-101.
17. Luton, J. A. and Mook, D. T., 1993, "Numerical simulations of flutter and its suppression by active control," AIAA Journal 31(12), 2312-2319.
18. Mook, D. T. and Dong, B., 1994, "Perspective: Numerical simulations of wakes and blade-vortex interaction," Journal of Fluids Engineering 116, 5-21.
19. Preidikman, S. and Mook, D. T., 1998, "On the development of a passive-damping system for wind-excited oscillations of long-span bridges," Journal of Wind Engineering and Industrial Aerodynamics 77-78, 443-456.
20. Rodden, W. P., Giesing, J. P., and Kalman, T. P., 1972, "Refinement of the nonplanar aspects of the subsonic doublet-lattice lifting-surface method," Journal of Aircraft 9(1), 69-73.
21. Strganac, T. W. and Mook, D. T., 1990, "A numerical model of subsonic aeroelastic behavior," AIAA Journal 28(5), 903-906.
22. Tang, D., Dowell, E. H., and Hall, K. C., 1999, "Limit cycle oscillations of a cantilevered wing in low subsonic flow," AIAA Journal 37(3), 364-371.
23. Tang, D., Dowell, E. H., and Virgin, L. N., 1998, "Limit cycle behavior of an airfoil with a control surface," Journal of Fluids and Structures 12, 839-858.
24. Thrasher, D. F., Mook, D. T., and Nayfeh, A. H., 1978, "Nonlinear dynamic-aerodynamic interaction," AIAA Atmospheric Flight Mechanics Conference, Palo Alto, CA, August, AIAA Paper No. 78-1346.