Limit-cycle stability reversal via singular perturbation and wing-flap flutter

Journal of Fluids and Structures

Volumn 19, Issue 6, 2004, Pages 765-783

  Dessi, D ^a   Mastroddi, F ^b  

^a ITALIAN SHIP MODEL BASIN   (Italy)

^b SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

BIFURCATION (MATHEMATICS); DEGREES OF FREEDOM (MECHANICS); ELASTICITY; INCOMPRESSIBLE FLOW; MATHEMATICAL MODELS; NONLINEAR SYSTEMS; PERTURBATION TECHNIQUES; RESONANCE;

ELASTIC MOMENTS; HOPF BIFURCATIONS;

FLUTTER (AERODYNAMICS);

AERODYNAMICS; AEROELASTICITY; FLUID-STRUCTURE INTERACTION; FLUTTER; INCOMPRESSIBLE FLOW; WING;

EID: 3042779505     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2004.04.010     Document Type: Article

References (20)

1. Alighanbari H. Lee B.H.K. Analysis of nonlinear aeroelastic signals Journal of Aircraft 40 2003 552-558
2. Alighanbari H. Price S.J. The post-Hopf bifurcation response of an airfoil in incompressible two-dimensional flow Nonlinear Dynamics 10 1996 381-400
3. Chen, P.C., Sarhaddi, D., Liu, D.D., 1998. Limit-cycle-oscillations studies of a fighter with external stores. AIAA Conference Paper with Number: AIAA-98-1727, pp. 258-266.
4. Conner M.D. Tang D.M. Dowell E.H. Virgin L.N. Nonlinear behavior of a typical airfoil section with control surface with freeplay: a numerical and experimental study Journal of Fluids and Structures 11 1997 89-109
5. Dessi D. Mastroddi F. Morino L. Limit-cycle stability reversal near a Hopf bifurcation with aeroelastic applications Journal of Sound and Vibration 256 2002 347-365
6. Dowell, E.H., Virgin, L.N., Tang, D.M., Conner, M.D., 1997. Nonlinear dynamics of aeroelastic systems. Proceedings of International Forum on Aeroelasticity and Structural Dynamics, Rome, Italy, 17-20 June, pp. 79-91.
7. Edwards J.W. Ashley H. Breakwell J.V. Unsteady aerodynamic modelling for arbitrary motions AIAA Journal 17 1979 365-374
8. Fung Y.C. An Introduction to the Theory of Aeroelasticity 1955 Wiley New York (reprinted by Dover, New York, 1969)
9. Guckenheimer J. Holmes P. Nonlinear Oscillations, Dynamical Systems, and Bifurcations of Vector Field 1983 Springer New York
10. Jones, R.T., 1940. The unsteady lift of a wing of finite aspect ratio. NACA Report 681.
11. Lacabanne, M., 1997. An experimental analysis of the aeroelastic behaviour with a freeplay in a control surface. Proceedings of International Forum on Aeroelasticity and Structural Dynamics, Rome, Italy, 17-20 June, pp. 79-91.
12. Lee B.H.K Gong L. Wong Y.S. Analysis and computation of nonlinear dynamic response of a two-degree-of-freedom system and its application in aeroelasticity Journal of Fluids and Structures 11 1997 225-246
13. Lee, B.H.K., Jiang, L., Wong, Y.S., 1998. Flutter of an airfoil with a cubic nonlinear restoring force. AIAA conference paper with number: AIAA-98-1725.
14. Lee B.H.K. Tron A. Effects of structural nonlinearities on flutter characteristics of the CF-18 aircraft Journal of Aircraft 26 1989 781-786
15. Mastroddi F. Bettoli A. Wavelet analysis for Hopf bifurcations with aeroelastic applications Journal of Sound and Vibration 225 1999 887-913
16. Matsushita, H., Mosekilde, E., Christiansen, L.E., Lehn-Schioler, T.L., Granasy, P., 2001. Examination of the two-degrees-of-freedom nonlinear math model for transonic flutter. Proceedings of International Forum on Aeroelasticity and Structural Dynamics, Madrid, 5-7 June, pp. 287-294.
17. Morino L. Mastroddi F. De Troia R. Ghiringhelli G.L. Mantegazza P. Matrix fraction approach for finite-state aerodynamic modelling AIAA Journal 33 1995 703-711
18. Nayfeh A.H. Balachandran B. Applied Nonlinear Dynamics 1994 Wiley New York
19. Theodorsen, T., 1935. General theory of aerodynamic instability and the mechanism of flutter. NACA Report 496, pp. 413-433.
20. Woolston D.S. Runyan H.L. Andrews R.E. An investigation of certain types of structural nonlinearities on wing and control surface flutter Journal of Aeronautical Sciences 24 1957 57-63