| 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. | 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 |
| 4. | 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。 |
| 5. | 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。 |
| 6. | In chapter 5 , a new dynamic wake model is developed by employing the rotor free - wake method in chapter 2 , and is used to investigate the curve distortion during the conversion of tiltrotor aircraft between helicopter flight conditions and airplane flight conditions
在第二章方法的基础上，第五章建立一个倾转旋翼动态尾迹模型，使用该模型对倾转旋翼机倾转过渡状态的尾迹弯曲变形进行了研究，得出了一些结论。 |
