propeller plane

1. The propeller of the plane is out of order, and is under repair.
   这架飞机的螺旋桨出了点问题，正在维修。
2. It took 13 hours on a propeller plane.
   一架螺旋桨飞机整整飞了13个小时。
3. They will eventually be permanently attached to the propeller shrouds and hull, and they will also house the stern plane hinge mechanism.
   他们最终会被永久地附加到螺旋桨整流罩和船体，他们也将内务严峻平面铰链机制。
4. Suddenly, according to an account in The Washington Post, the crowd saw a little propeller plane buzzing along with a sleek fighter jet flying circles around it.
   突然，据华盛顿邮报的话说，观众们看见一架小螺旋桨飞机嗡嗡飞来，身旁盘旋着一架光滑抢眼的喷气式战斗机。
5. The disadvantages would be engine cooling plus an ejecction system or propeller jettison would have to be designed for the pilot to safely exit the plane in case of an emergency.
   劣势在于引擎冷却的问题，还有喷气系统和螺旋桨的抛弃要设计得符合紧急情况下飞行员逃生的安全性。
6. Results showed that the height of propeller from bottom sediment, water velocity on the jet exit, diameter of propeller are main factors acting on flow velocity on the bottom plane.
   结果表明，螺旋桨距河流底面的深度、螺旋桨射流出口流速、螺旋桨直径对底部流速的分布影响显著；
7. Special interfaces are designed to control AUV's propeller, plane and rudder with the drivers of motors.
   控制器中设计了专用接口电路，配合电机驱动器控制水下自航行器的推进器和航向部件。
8. In order to reveal the developing law of propeller slipstream and the interference on different components of plane, It is necessary to accurately measure different cross section flow parameters in the slipstream region and to study the influence on surface pressure of different component plane.
   为了揭示螺旋桨滑流的发展规律和滑流对飞机各部件的干扰机理，很有必要精确测量滑流区不同截面的流动参数，研究滑流对飞机各部件表面压力的影响。
9. In this paper, the result of wind tunnel test for a powered ground effect plane model with propeller was introduced. The influence of ground effect and rotative velocity of the propeller on aerodynamic properties of this plane was also presented.
   介绍地效飞机带螺旋桨动力模型的风洞试验结果，着重介绍地面效应和螺旋桨转速参数对飞机气动力特性的影响。
10. Considering that the propeller matches the motor/ rotor and integrates with the motor/ rotor in the structure, by using plane straight arrayed lamina bar theory, I design and calculate structure parameters of the propeller.
    在兼顾推进器与电机的匹配和结构一体化，采用平面直列叶栅理论，设计计算了推进器的结构参数。
11. The methods were studied for predicting range and endurance of a propeller plane at constant altitude.
    研究了螺旋桨飞机等高度飞行时航程、航时的计算方法。
12. The nonuniformity coefficients were presented to estimate wake flow field at the propeller disk plane in three components.
    特别针对受到主要关注的推进器所在剖面的三向伴流场，借助流场不均匀度系数，给出了直观的定量评估。

noun

1. an airplane that is driven by a propeller