| 1. | Critical velocity of ultra - fine comminuting coal with dia - jet
前混合水射流超细粉碎煤粒的临界速度 |
| 2. | Both h controller and synthesis are designed when the damping uncertainties in plunge
在稍大于颤振临界速度的风 |
| 3. | Supercritical velocity of flow
怜的超临界速度 |
| 4. | Critical locking speed
锁止临界速度m s |
| 5. | A linear saturated law is used to restrain flutter . the critical velocity can be improved more than 30 %
实现了颤振的主动抑制，可以将原有气动弹性系统的临界速度提高30以上。 |
| 6. | The critical velocity at which the bird body impacts the glass at middle point to result in break of the glass is 570 - 580km / h
鸟撞飞机圆弧风挡玻璃的中点时风挡玻璃发生破碎的临界速度约为570 ? 580km h 。 |
| 7. | 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 % 。 |
| 8. | The definitions of two critical speeds of the target ( undetectable speed and partially detectable speed ) are given , and the functional relation between these two speeds and sensor parameters are presented
据此分析了目标的速度与检测可能性之间的关系，给出了不可测临界速度和部分可测临界速度的定义及其与传感器参数之间的函数关系。 |
| 9. | Numerical results are in good agreement with some data and the method and procedure presented in this paper are verified . and then the wing ? flutter characters of a missile wing are numerical simulated with the examples of a missile wing
以某导弹翼面为算例，对弹翼的亚、跨、超音速的颤振临界速度进行了数值计算，部分计算结果与风洞计算结果相比较，一致性很好。 |
| 10. | When the target speed is greater than the undetectable speed , the sensor can ' t detect the target , and when the target speed is greater than the partially detectable speed and moves backward to the sensor , the sensor can ' t detect the target
当目标的速度大于不可测临界速度时，传感器无法测量目标；当目标背离传感器运动，并且速度大于部分可测临界速度时，传感器无法测量到目标。 |
