1. In order to eliminate the interaction between aeroelasticity and flight control of vehicles, the positions of mounted sensors must be chosen properly.

2. There exist obvious aeroelasticity problem for the large-scaled civil aircraft with high aspect ratio wings.

3. Develop an analytical model of the nonlinear aeroelasticity of the high-aspect-ratio wings and give the nonlinear partial equations of wing structure motion based on the Hamilton principle.

4. A method of analysis of the effect of aeroelasticity on the stability of elastic vehicles by using a simplified mathematical model of unsteady aerodynamic forces is proposed.

5. In this paper, based on theory of aeroelasticity, the mathematical model of rotor of labyrinth seal flow induced vibration, dynamical behaviors of the rotor system are analyzed.

6. There are many new problems of aeroelasticity which are introduced by the novel concepts and system characteristics in the design process of hypersonic vehicles.

7. The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.

7. try its best to gather and create good sentences.

8. The longitudinal stability of elastic vehicles is studied with the effect of aeroelasticity considered.

9. Some typical numerical results are presented from application of the model to the static analysis, dynamic analysis, static aeroelasticity and flutter analysis of a wing-box and a wing.

10. Airfoil flutter is one of the important problems in aeroelasticity.

11. However, this new structure also leads to some problems in strength and aeroelasticity , so some analytical results and suggestions are presented.

12. Coupled with the structural equations, the models for transonic aeroelasticity in state - space are got.

13. In this paper, we studied identification of a kind of integro-differential equations to describe unsteady aerodynamics and aeroelasticity phenomenon.

14. Inertia relief theory and static aeroelastic method based on CFD/CSD are introduced in this paper. Three force equilibrium methods of static aeroelasticity are compared with.

15. With simplified unsteady aerodynamic force mathematical model, method of analysis for the effects of aeroelasticity on the dynamic stability of elastic vehicles is established.

16. Realizing data exchange to reflect coupling between fluid and structures is essential to solving static aeroelasticity problems.

17. Some typical numerical results are presented from application of the model to static analysis, dynamic analysis, static aeroelasticity and flutter analysis of a wing-box and a wing.