thrust on的例句大全

Experimental investigation on lox/ propane thrust chamber

液氧/丙烷推力室试验研究

Research of damage mitigating control of thrust chamber based on fuzzy logic reasoning for liquid propellant rocket engine

基于模糊推理的液体火箭发动机推力室减损控制研究

Effect of aspect ratio on heat transfer and fluid flow in regenerative cooling channel of liquid rocket engine thrust chamber

通道深宽比对液体火箭发动机推力室再生冷却的影响

The primary analysis on heat transfer and pressure drop of the thrust chamber in hydrogen-oxygen-hydrocarbon tripropellant rocket engine

氢氧烃三组元发动机燃烧室传热、流阻初步分析

Study on thrust characteristic of linear induction motor of the high-speed maglev vehicle by using equivalent circuit method

高速磁浮动车直线电机推力特性的等值电路法

Based on the simulation result, the similarity law of respective factor which has influenced cogging force and thrust characteristic is analyzed.

对比分析这些参数对齿槽定位力和推力特性影响的相似性规律。

Based on the combination approach of analysis method and finite element simulation, This paper has researched the similarity of structure and thrust characteristic of Brushl.

本文通过解析分析和有限元计算相结合的方法对无刷直流直线电机的结构和推力特性方面进行相似性分析。

Results show that the highest place of flux density is superposition of armature and guide sleeve end of pole piece, and the changing for pole piece inside diameter unilateral gap settle on the thrust characteristic.

通过可视化模拟和分析得知，磁通密度最高的地方是衔铁与极靴导套端重叠部分，极靴内径单侧间隙的变化对吸力起决定作用。

Calculating thrust coefficient and torque coefficient of propeller properties across four quadrants based on Matlab

螺旋桨的四象限推力系数和转矩系数的Matlab实现方法

The effect of operation pressure on the specific impulse of tactical missile solid motors is analyzed from several factors, such as characteristic velocity, thrust coefficient, impulse coefficients of the chamber and nozzle.

从固体发动机的特征速度、推力系数、燃烧室冲量系数和喷管冲量系数等因素出发，分析了发动机工作压强对战术固体火箭发动机比冲的影响。

Based on the previous computation for a rotor flow field in forward flight near ground, the thrust coefficient, torque coefficient and blade flapping angles are calculated and analysed against the advance ratios and flight heights.

基于对旋翼近地飞行时流场的N－S方程计算，计算并讨论了近地飞行时，旋翼拉力、扭矩系数及桨叶挥舞角随前进比、离地高度的变化情况。

The scale effect on thrust deduction coefficient is small, which may be con-sidered approximately constant for models greater than 5 meters in length.

推力减额分数的尺度效应较小，当船模长度大于5米时可视力常数。

Analyzed the severe corrosion for the cause and mechanism occurring on the thrust runner and spacer as well thrust collar from one plant, and presented protecting measures, discussed its construction also.

从某电站发生推力头、垫片和镜板严重腐蚀，分析其原因和机理，并提出防护措施及结构探讨。

On the basis of above, a fuzzy logic control system with self regulating control rules and nonlinear parameter optimization is proposed so as to improve the performances of modern integrated flight/ thrust control system with constant attack angle.

在此基础上，提出了APCS采用控制规则在线自调整及非线性参数优化的模糊逻辑控制。

Carrier Landing Flight/ Thrust Control System Based on Intelligent Design Software

基于智能软件的着舰飞行/推力控制系统

The Maximum Thrust Control of Linear Induction Motor Based on SVPWM

基于空间矢量PWM的直线感应电机的最大推力控制

Direct Thrust Control of Interior Permanent Magnet Linear Synchronous Motor Based on Voltage Estimation

基于电压预测的直线永磁同步电机直接推力控制

The inverse model control method is proposed based on the control structure design and used in aeroengine thrust control system.

提出了基于控制结构设计的模型逆控制方法，用于航空发动机直接推力控制系统。

Then, based on PID arithmetic, the closed loop control program for thrust control system was designed.

然后基于PID算法，对推力控制系统进行闭环程序设计。

A direct thrust control system based on sliding mode controller is developed, which has a insensitive trait and strong robustness for parameter.

将具有参数变化不敏感、系统鲁棒性强的滑模变结构控制技术引入其中，构成一种基于滑模变结构控制器的直接推力控制系统。