| 1. | Tiltrotor aircraft key technology developing research
倾转旋翼飞机技术发展研究 |
| 2. | Flight control system development for the xv - 15 tiltrotor aircraft
15倾转旋翼飞机飞行控制系统概述 |
| 3. | Mathematical model and formulations of a new tilt - rotor aircraft for aeroelastic stability analysis
新型倾转旋翼机气动弹性稳定性分析模型 |
| 4. | The application of parameter space method in design of flight control system for tiltrotor aircraft
参数空间法在倾转旋翼机飞行控制系统设计中的应用 |
| 5. | The multi - body analysis of the aeroelastic stability of the tiltrotor aircraft is presented
摘要通过多体动力学方法建立了倾转旋翼机动力学分析模型。 |
| 6. | The rotor / wing aerodynamic interactions of the tilt rotor vehicle in hover is described in this dissertation
本文主要研究的是倾转旋翼飞行器悬停状态时，旋翼机翼之间的气动干扰问题。 |
| 7. | 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。 |
| 8. | When the tilt rotor vehicle is in hover , the aerodynamic download of the rotor flowfield imposes on the wing . in this time , the rotor / wing interaction is severe
倾转旋翼飞行器悬停时，旋翼的下洗流刚好作用在机翼上，此时，旋翼机翼间的气动干扰非常剧烈。 |
| 9. | Numerical simulations demonstrate that the multi body analytical model can analyze the aeroelastic stability of the tiltrotor aircraft in the helicopter mode
数值计算表明：建立的多体动力学模型能够快速分析直升机模式下倾转旋翼机复杂的旋翼机翼气弹耦合动力学特性。 |
| 10. | Multi body dynamic differential equations are combined with the equations of the unsteady dynamic inflow model to establish the complete unsteadily aeroelastic coupling analytical model of the tiltrotor
结合动力人流，研究了直升机模式下倾转旋翼机非线性非定常气弹耦合动力学特性。 |
