近些年来，人们开始应用计算流体动力学（CFD）来求解气动弹性问题。
Years followed, current research has turned toward the application of Computational Fluid Dynamics(CFD) models to the solution of these aeroelastic problems.
耦合结构动力学方程，建立了基于状态空间的跨声速气动弹性分析模型。
Coupled with the structural equations, the models for transonic aeroelasticity in state-space are got.
将等效板模型推广应用到典型机翼结构的静力学、动力学以及静、动气动弹性分析中。
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.
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