Assessment of added mass effects on flutter boundaries using the Leishman-Beddoes dynamic stall model

Journal of Fluids and Structures

Volumn 26, Issue 5, 2010, Pages 814-840

  Peiro J ^a   Galvanetto, U ^a,b   Chantharasenawong, C ^a,c  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

^b UNIVERSITY OF PADOVA   (Italy)

^c KING MONGKUT'S UNIVERSITY OF TECHNOLOGY THONBURI   (Thailand)

Author keywords

Added mass effects; Aeroelasticity; Dynamic stall; Flutter boundaries; Nonlinear dynamics; Stall flutter

Indexed keywords

ADDED MASS; DYNAMIC STALL; FLUTTER BOUNDARIES; NON-LINEAR DYNAMICS; STALL FLUTTER;

AEROELASTICITY; AIRFOILS; DYNAMICS; ELASTIC WAVES; HOPF BIFURCATION; ORDINARY DIFFERENTIAL EQUATIONS; STALL INDICATORS;

FLUTTER (AERODYNAMICS);

EID: 77955656738     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2010.04.002     Document Type: Article

References (27)

1. Beddoes T. A synthesis of unsteady aerodynamic effects including stall hysteresis. Vertica 1976, 1:113-123.
2. Beddoes T. Representation of airfoil behaviour. Vertica 1983, 7(2):183-197.
3. Beddoes T. Practical computation of unsteady lift. Vertica 1984, 8(1):55-71.
4. Beedy J., Barakos G., Badcock K., Richards B. Non-linear analysis of stall flutter based on the ONERA aerodynamic model. Aeronautical Journal 2003, 495-509.
5. Blevins R.D. Flow-induced Vibration 2001, Krieger Pub. Co., Malabar, Florida. second ed.
6. Chantharasenawong, C., 2007. Nonlinear aeroelastic behaviour of aerofoils under dynamic stall. Ph.D. Thesis, Department of Aeronautics, Imperial College London.
7. Crouse G.J., Leishman J. Transonic aeroelasticity analysis using state-space unsteady aerodynamic modeling. Journal of Aircraft 1992, 29(1):153-160.
8. Dat R., Tran C. Investigation of the stall flutter of an airfoil with a semi-empirical model of 2-D flow. Vertica 1983, 7(2):73-86.
9. Fung Y.C. An Introduction to the Theory of Aeroelasticity 1993, Dover, New York.
10. Galvanetto U., Peiró J., Chantharasenawong C. Remarks on the nonlinear dynamics of a typical aerofoil section in dynamic stall. Aeronautical Journal 2007, 111(1125):731-739.
11. Galvanetto U., Peiró J., Chantharasenawong C. An assessment of the effect of non-smoothness of the Leishman-Beddoes dynamic stall model on the nonlinear dynamics of a typical aerofoil section. Journal of Fluids and Structures 2008, 24:151-163.
12. Guckenheimer J., Holmes P. Nonlinear oscillations, dynamical systems, and bifurcations of vector fields. Applied Mathematical Sciences 2002, vol. 42. Springer, New York.
13. Hansen, M.H., Gaunaa, M., Madsen, H.A., June 2004. A Beddoes-Leishman type dynamic stall model in state-space and indicial formulation. Technical Report RISO-R-1354, Risø National Laboratory, Roskilde, Denmark.
14. Lee B., Price S., Wong Y. Nonlinear aeroelastic analysis of airfoils: bifurcation and chaos. Progress in Aerospace Sciences 1999, 35:205-334.
15. Leishman, J., 2006. Principles of Helicopter Aerodynamics, second ed. Cambridge.
16. Leishman, J., Beddoes, T., 1986. A generalised model for airfoil unsteady aerodynamic behaviour and dynamic stall using the indicial method. In: Proceedings of the 42nd Annual Forum of the American Helicopter Society, Washington, DC.
17. Leishman J., Beddoes T. A semi-empirical model for dynamic stall. Journal of the American Helicopter Society 1989, 34:3-17.
18. Leishman J., Nguyen K. State-space representation of unsteady airfoil behaviour. AIAA Journal 1988, 28(5):836-844.
19. Li X., Fleeter S. Dynamic stall generated airfoil oscillations. International Journal of Turbo and Jet Engines 2003, 20:217-233.
20. Mahajan A., Kaza K., Dowell E. Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter. Journal of Fluids and Structures 1993, 7:87-103.
21. McAlister, K., Pucci, W., McCroskey, W., Carr, L., September 1983. An experimental study of dynamic stall on advanced airfoil sections; volume 2 pressure and force data. NASA Technical Memorandum TM-84245.
22. McCroskey W., Carr L., McAlister K. Dynamic stall experiments on oscillating airfoils. AIAA Journal 1976, 14(1):57-63.
23. Price S., Fragiskatos G. Nonlinear aeroelastic response of a two-degree-of-freedom airfoil oscillating in dynamic stall. 7th International Conference on Flow Induced Vibration, Lucerne, Switzerland 19-22 June 2000, 437-444. A.A. Balkema, Rotterdam. S. Ziada, T. Staubli (Eds.).
24. Price S., Keleris J. Non-linear dynamics of an airfoil forced to oscillate in dynamic stall. Journal of Sound and Vibration 1996, 194(2):265-283.
25. Sarkar S., Bijl H. Nonlinear aeroelastic behaviour of an oscillating airfoil during stall-induced vibration. Journal of Fluids and Structures 2008, 24:757-777.
26. Tang D., Dowell E. Comments on the ONERA stall aerodynamic model and its impact on aeroelastic stability. Journal of Fluids and Structures 1996, 10(4):353-366.
27. Tran C., Petot D. Semi-empirical model for the dynamic stall of airfoils in view to the application to the calculation of responses of a helicopter blade in forward flight. Vertica 1981, 5:35-53.