Measurement of Solid-Gas Phase Flow Using Flight Time of Peak

Theoretical exploration and practical evaluation of the flight time calculation method of counter movement jump height

纵跳高度腾空时间计算法的理论探讨与实验评价

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Time scale up can stretch the entire flight time by a factor of 1 000 and then the stretched result is counted to calculate the distance.

利用时间比例放大法可以把激光脉冲往返于测程之间的时间按比例放大1000倍，放大后的结果用于计算被测距离。

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Your exact flight time may vary depending on wind speeds.

您的具体飞行时间可能会有所变化，这取决于风速。

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Minimum Flight Time for Sino-American Airline Across the North Pole

中美航线飞越北极最短时间

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An algorithm for finding projectile flight time by solving the trajectory equations

求解目标点弹丸飞行时间的一种快速算法

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What's the actual flight time from here to Moscow?

从这里到莫斯科的实际飞行时间是多少？

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Using penetration probability as the evaluation criterion, the validity of random maneuver strategy with the flight time in normal distribution is discussed.

以突防概率为评价标准，研究了突防持续时间在正态分布情况下随机机动策略的有效性。

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The conception of equivalent mass is introduced in the calculation of flight time and its physical meaning and mathematical implication are explained.

在飞行时间的计算中，引入了相当质量的概念，并说明了它的物理和数学的含义。

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Measurement of tritium depth profile by flight time method

用飞行时间法测量氚的深度分布

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A high-resolution flight time measurement system based on a single field programmable gate array ( FPGA) in laser altimeter is designed.

设计了在激光测高系统中基于单芯片现场可编程门阵列（FPGA）的高精度时间间隔测量模块。

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The limits of initial velocity and flight time of landing moon orbit;

登月轨道初速及飞行时间限制；

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The Measurement of Flight Time for Pulsed Laser Ranging Based on CPLD

基于CPLD的脉冲激光测距飞行时间测量

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The experiment result indicates that the system is stable and can satisfy the requirement of acoustic wave flight time measurement.

实验结果表明该测量系统性能稳定，能满足声波飞行时间测量系统的要求。

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Design and realization of the acoustic waves flight time measurement system based on cross-correlation method

基于互相关技术的声波飞行时间测量系统的设计与实现

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The influence of the experimental conditions on the flight velocity of the ejected plasma was discussed based on the feature of their time-of-flight spectra.

结果表明，在脉冲激光沉积薄膜的情况下，喷射等离子体的飞行速度主要依赖于作用于靶面的激光能量密度。

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The model's flight velocity is 4.8~ 5.7km/ s, and the chamber's pressure is 10~ 80mmHg.

球模型飞行速度为4.8～5.7km／s，靶压10～80mmHg。

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The mathematic model equations, boundary conditions and nonlinear iterative algorithm established herewith can be used to calculate the variations of flight path, velocity ( or angular velocity), acceleration as well as load factor, etc, with time for the said maneuvers.

所建立的数学模拟方程、边界条件以及非线性迭代求解方法，可以用来计算该机动科目的飞行轨迹、速度（或角速度）、加速度以及载荷因数等随时间的变化。

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A new method of flight velocity recognition of low-velocity projectile

低速弹飞行速度识别的一种方法

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Finally, the working loading spectra are calculated from altitude velocity characteristic, flight altitude and flight velocity.

最后根据发动机的高度&速度特性计算出发动机的工作参数谱。

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To deal with the situations of close flight and cross flight, the velocity information of targets and the method of partly processing are taken into track correlation.

针对近飞目标和交叉飞行目标的情况，点迹与航迹的关联采用了分块处理技术，并融合了目标的速度信息。

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