| 1. | The dynamic loads must be extrapolated using aeroelatic scale factors .
动力载荷必须用气动弹性尺度因子来推算。 |
| 2. | 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。 |
| 3. | Study on stability and manoeuvrability of flying wing aircraft
大展弦比机翼的气动弹性问题探讨 |
| 4. | The computed flutter speeds are within 10 % of experimentally determined ones
并在时间域内分析了高超音速气动弹性的非线性。 |
| 5. | In the thesis , an energy analysis method is applied to study the buzz
在气动弹性问题方面，本文采用能量法分析和研究了嗡鸣。 |
| 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. | Design method of active control law based on reduced order model of unsteady aerodynamics for aeroelasticity
基于非定常气动力低阶模型的气动弹性主动控制律设计 |
| 9. | 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。 |
