An analysis method of loads on aircraft elastic wing with its real deformation considered 方程的弹性机翼载荷分析方法研究
2.
The stability of the tiltrotor in the heli copter mode is analyzed aiming t a semi span soft - inplane tiltrotor model with an elastic wing 集成了非定常动态人流方程与倾转过渡状态的多体动力学力程，建立了倾转旋翼机时域非定常气弹耦合分析模型。
3.
The research of this dissertation is focused on how to solve the 3 - dimensional compressible navier - stokes equations by the implicit finite difference algorithm and to simulate numerically the unsteady subsonic and transonic viscous flows around rigid and elastic wings . on the base of them the aeroelastic characterictics of an elastic wing have been studied 本文的主要工作是用隐式有限差分法求解三维非定常紊流n - s方程组，数值模拟刚性机翼及弹性机翼的亚、跨、超音速定常及非定常粘性绕流，并在此基础上研究了弹性机翼的气动弹性问题。
