Aeroelastics should be developed as a decisive role during the period of airplane design. 气动弹性作为一门设计学科应在设计过程中发挥关键性作用。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft. 在气动弹性领域中，人们在设计过程中最为关心的是颤振现象。
On this base, the static aeroelastics problems of wing and aircraft are investigated by coupled with structure dynamic equation. 并在此基础上耦合结构力学方程研究了三维机翼以及全机的静气动弹性问题。
On the base of the numerical simulation of unsteady viscous flows, the characters of the static aeroelastics and flutter for the wings are researched. 在模拟非定常粘性绕流的基础上，对涉及机翼和控制面流固耦合作用的静气动弹性特性和颤振特性进行了研究。
Servo aeroelastics analysis is becoming more and more important in designing modern surface-to-air and air-to-air missiles when high velocity and super maneuverability were needed. 随着对飞行速度和机动性能要求的不断提高,伺服气动弹性问题成为新一代地空和空空导弹急需解决的重要技术问题。
