Sink low to generate maximum thrust. Use your arms to assist and "steer."
放低身体以产生最大的冲力，再用你的双手加强动力并引导方向。
The new kind of design allows the complete balancing of the guide rail at maximum thrust.
这种新设计保证导轨在最大推力下保持平衡。
In this paper, employing rigorous variational calculus, equations of control surface at maximum thrust nozzle exit are derived.
本文用严格的变分法导出了最大推力喷管出口控制面方程。
The condition of the existence of solution of functional extreme value problem applied to maximum thrust nozzle is also presented.
同时，还导出了最大推力喷管这个泛函极值问题解存在的条件。
In general, the piezoelectric linear motor is defined by no load velocity, the maximum thrust force, efficiency and other parameters.
一般用空载速度、最大推进力、效率及其他一些参数来表征压电线性马达。
There exists an optimal exit area of secondary nozzle to result in a maximum thrust of rocket ejector in the light of the investigated ejector chamber structure.
在文中所研究的引射燃烧室结构条件下，存在一个最佳二次喷管出口面积，它能使引射火箭的推力达到最大。
The stable motor control was introduced to the maximum thrust control by using this strategy. The velocity control was realized through the control of electromagnetic thrust Angle.
该控制策略将直线电机的稳定控制引入到最大推力控制中，通过控制电机的电磁力角，实现直线电机的速度控制。
Altitude CAPABILITY, the maximum altitude at which the airplane can be flown at for a given thrust, speed and atmosphere condition.
高度能力，在给定的推力，速度和大气状况下，飞机能飞达的最大高度。
The thrust limitation explains why it is always appropriate to use the maximum diameter available to maximize output torque.
推力限制解释了为什么它总是适当使用最大直径可最大限度地输出扭矩。
With such a pressure ratio of 5, the resulting thrust is about 60% of maximum theoretical.
与这样的压力比5，由此产生的推力是约60 %的最高理论。
The test result shows that maximum tolerance of the simulated ambient pressure deviation is about 14% under which the engine thrust uncertainty remains less than 1.0%.
试验结果表明，在保证推力不确定度优于1.0%的条件下，拉瓦尔喷管发动机高空模拟试验的模拟偏差容限约为14%。
Finally, a brief discussion is present about the influence of the airplane gross weight, the thrust, the maximum Angle of attack, the flap Angle and the wind over the deck on...
最后讨论了飞机的起飞质量，发动机推力、起飞迎角、襟翼偏角和甲板风航迹等对弹射起飞性能的影响。
Finally, a brief discussion is present about the influence of the airplane gross weight, the thrust, the maximum Angle of attack, the flap Angle and the wind over the deck on...
最后讨论了飞机的起飞质量，发动机推力、起飞迎角、襟翼偏角和甲板风航迹等对弹射起飞性能的影响。
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