| 1. | Physical modeling of atmospheric boundary layer wind tunnel experiment
大气边界层风洞实验的物理模型 |
| 2. | Wind tunnel experiment on the model of the chinese national grand theatre
中国国家大剧院模型风荷载风洞实验 |
| 3. | Flutter stability of long span self - anchored suspension bridges and wind - tunnel tests
大跨度自锚式悬索桥的颤振稳定性研究及风洞实验 |
| 4. | The wind - tunnel investigation of the characteristics and mechanism of twin - vertical tail buffet of leading - edge extension configuration
边条翼布局双垂尾抖振特性与机理风洞实验研究 |
| 5. | Abstract : the dynamic stall experiment is an unsteady aerodynamic test , whose experimental data are random
文摘:动态失速风洞实验是一种非定常实验，其测量所得数据属于随机数据范畴。 |
| 6. | Wind tunnel test , as the one of general means of aerodynamic research , is very important and high effective
风洞实验作为空气动力学研究的基本手段之一，是非常重要的，也是非常有效的。 |
| 7. | The optimized heat exchangers module was verified to be good based on wind tunnel test and road test
改进方案的风洞实验和实车路试结果表明，各散热器的散热量达到设计指标，各系统工作正常。 |
| 8. | As one part of wind tunnel test , test system ' s performance will effect directly the schedule of wind tunnel test and the following works
测试系统作为风洞实验重要组成部分之一，其性能的优劣，直接影响着风洞实验进度及其后续工作。 |
| 9. | Low speed wind tunnel experiment requires strict of the wind speed , which requires a wild range of wind speed , high precision , and quick adjustment
低速风洞实验要求对实验段的风速有严格的控制，要求风速调节范围宽，精度指标高，调节速度快。 |
| 10. | The numerical simulations agree well with the wind the tunnel experiments , and the critical speed is increased by 13 . 4 % . chapter 5 presents the robust flutter suppression of the airfoil
数值仿真和风洞实验表明,这两种控制器是有效的,可将系统的颤振临界速度提高23 . 4 % 。 |
