| 1. | The aeroelastic phenomena may be subdivided under the heading static and dynamic .
气动弹性现象可以再分为静态和动态两个专题。 |
| 2. | Aeroelastic analysis of flexible large aspect ratio wing
特大展弦比机翼的特性与设计 |
| 3. | Wind tunnel studies on the behaviour of aeroelastic twin cable model
串列双索气弹模型的风洞试验研究 |
| 4. | Structural modeling and aeroelastic analysis of high - aspect - ratio composite wings
飞翼飞机稳定性与操纵性研究 |
| 5. | An effective transonic inverse design method for aeroelastic wing
基于控制理论方法的跨声速弹性机翼反设计方法研究 |
| 6. | The different influences of temperature to two aeroelastic systems are analyzed
分析了温度对这两种热结构气动弹性系统的不同影响。 |
| 7. | 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 |
| 8. | 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。 |
| 9. | Model experiment and damping identification for aeroelastic stability of helicopter rotor with elastomeric lag damper
带粘弹减摆器旋翼系统气弹稳定性试验与阻尼识别 |
| 10. | Finally for all the above aeroelastic problems , distributed parallel computation is accomplished
最后对以上气动弹性问题的数值计算进行了基于微机网络的分布式并行计算研究。 |
