By the use of an unsteady Euler or Navier-Stokes CFD algorithm coupled with a Computational structural dynamics(CSD)solver,the complete aeroelastic response of the structure can be preliminary predicted.

• 通过使用非定常的欧拉或Navier-Stokes(N-S)方程的CFD计算技术和计算结构动力学(CSD)的耦合，对飞行器结构的整个气动弹性响应可以初步预测。