Comments on the ONERA stall aerodynamic model and its impact on aeroelastic stability

Journal of Fluids and Structures

Volumn 10, Issue 4, 1996, Pages 353-366

  Tang, D M ^a   Dowell, E H ^a  

^a Duke University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROELASTICITY; FLUTTER;

EID: 0029857576     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1006/jfls.1996.0023     Document Type: Article

References (10)

1. DOWELL, E. H. 1995 Eigenmode analysis in unsteady aerodynamics: reduced order models. Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, New Orleans, LA, April, 1995. To be published in the AIAA Journal.
2. DUNN, P. & DUGUNDJI, J. 1992 Nonlinear stall flutter and divergence analysis of cantilevered graphite/epoxy wings. AIAA Journal 30, 153-162.
3. MEIJER, J. J. & CUNNINGHAM, A. M., JR. 1995 A semi-empirical unsteady nonlinear aerodynamic model to predict transonic LCO characteristics of fighter aircraft. Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, New Orleans, LA, April, 1985.
4. PETERS, D. A. 1985 Toward a unified lift model for use in rotor blade stability analyses. Journal of the American Helicopter Society 30, 32-42.
5. PETOT, D. 1989 Differential equation modeling of dynamic stall. La Recherche Aerospatiale 5, 51-64.
6. TANG, D. M. & DOWELL, E. H. 1992a Chaotic stall response of a helicopter in forward flight. Journal of Fluids and Structures 6, 311-335.
7. TANG, D. M. & DOWELL, E. H. 1992b Flutter and stall response of helicopter blade with structural nonlinearity. Journal of Aircraft 29, 953-960.
8. TANG, D. M. & DOWELL, E. H. 1993a Comparison of theory and experiment for nonlinear flutter and stall response of a helicopter blade. Journal of Sound and Vibration 162, 251-276.
9. TANG, D. M. & DOWELL, E. H. 1993b Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade. AIAA Journal 31, 1133-1142.
10. TRAN, C. T. & PETOT, D. 1981 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 5, 35-53.