The better static thrust will improve take-off performance.
较好的静推力将提高起飞性能。
Having decent static thrust, and reasonable speed capability.
有体面的静推力，合理的速度和能力。
The 11X4 or 12X3 are propellers which give great static thrust, at the cost of top speed of the airplane.
在11X4和12X3的螺旋浆起到极大的静态推力的飞机的最高速度为代价。
This would sacrifice "static thrust" (the pull when the plane is stationary on the runway) for thrust at high airspeed.
这将牺牲“静态推力”高空速(拉时的推力，飞机在跑道上固定)。
NOTE: Valves are static grounded by thrust washer and packing.
注意：这些阀门通过止推垫圈和填料实现静电接地。
Note: Valves are static grounded by thrust washer.
注意：这些阀门采用止推垫圈实现静电接地。
Also, the calculation formula of the contact stress, the fatigue strength and the static strength for the small thrust bearing which are attached at the end face of roller are derived.
同时又对滚子端面的小型推力球轴承推导出接触应力、疲劳强度和静载强度的计算公式。
A piezoelectricity measuring system used for measuring rocket thrust vector is introduced. A devices to static accomplish, calibration and dynamic calibration on the system is designed.
重点介绍了一种用于测量火箭发动机推力矢量的压电式测试系统，并设计了对测试系统进行静态标定和动态标定的装置。
Firstly, measuring principle of the thrust measuring system is introduced, and how to select the design schemes of static calibration.
首先，本文介绍了轨控发动机推力矢量测试原理，及静态标定装置设计方案的选择。
In this thesis, the Finite Element Method is applied to the solution of the Laplace equation formulated by means of stream function for the calculation of the static hydraulic thrust.
本文通过有限元法求解用流函数表示的拉普拉斯方程，进而计算轴流式机组的静态轴向水推力。
In this papers, I drew a series of thrust and vertical force curve of linear motor by measure them in vary condition. Then, its static characteristic is gained and a theory analysis is made.
文章通过对直线电机在各种条件下所受的法向力与垂直力的测量，得出一系列电流-法向力、垂直力，频率-法向力、垂直力曲线，推出直线电机静态特性，并对其进行了理论分析。
This plot of the thrust-time curve for the B-200 motor was made using data collected from a static firing on the static Test Rig.
这个阴谋的主旨-时间曲线为b - 2 00型汽车是用收集到的数据从一个静态射击对静态试验台。
The liquid used has zero-degree-static-contact angles on the semispherical container and is exposed to an initially concave interface in a zero-g environment before thrust.
所用液体与半球形箱壁之间的接触角为零并在加载前形成了失重初始凹液面。
The liquid used has zero-degree-static-contact angles on the semispherical container and is exposed to an initially concave interface in a zero-g environment before thrust.
所用液体与半球形箱壁之间的接触角为零并在加载前形成了失重初始凹液面。
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