yawing

英 [ˈjɔːɪŋ]

美 [ˈjɔːɪŋ]

v.  偏航
yaw的现在分词

现在分词：yawing　

柯林斯词典

• VERB （飞机或船）偏航，偏离航线
  If an aircraft or a shipyaws, it turns to one side so that it changes the direction in which it is moving.
  1. As the plane climbed to 370 feet, it started yawing...
     飞机攀升到370英尺时，开始偏航。
  2. He spun the steering-wheel so that we yawed from side to side.
     他急速打着舵轮，把我们搞得摇来晃去的。

双语例句

• Combined with the characteristic of vehicle walking mechanism and track line, the geometry relation and dynamics relation among air spring, yawing and tack is described with mathematical formulas.
  结合车辆走行机构和线路轨道的结构特点，对空气弹簧、转向架和轨道之间的几何关系和动力学关系进行了数学描述。
• Yawing moment of inertia of sprung mass
  簧上质量横摆惯性矩
• The normal force, pitching and yawing moments on the fuselage in hover result from the rotor downwash.
  悬停时，下洗尾流使机身产生负升力、俯仰力矩和偏航力矩。
• In the paper, the relation between cable vibration acceleration and wind velocity, wind yawing anger, anger of attack are discussed. Nonstationarity in wind-rain induced response is studied, and the cause of this nonstationarity is discussed by using a wavelet approach.
  分析了拉索振动加速度信号与风速、风偏角以及风攻角的相关性；研究了斜拉索振动加速度信号的非平稳性，并使用小波分析的方法探讨了导致其非平稳的原因。
• The effect of the primary longitudinal and lateral stiffness on the yawing of independent wheels is researched, and the reasonable range of values of the primary horizontal stiffness is obtained.
  研究了一系纵向和横向刚度对轮对摇头振动的影响，得出了一系水平刚度的合理取值范围。
• In each mode, it includes four attitude controls: rolling, pitching, yawing and thrust.
  在各种飞行模式下包含有四种姿态控制：滚动、俯仰、偏航和升降。
• Physical model experiments were made to obtain the observed data of yawing range, yawing period and mooring force of3 ship types under different working conditions.
  通过物理模型试验，得到了3种船型在不同工况组合下的偏荡幅度、偏荡周期以及系泊力实测数据。
• This paper describes the characteristics of rotating and yawing damping moment of wraparound fins in sub-supersonic flow and theoretically proves the necessity of positive-opposite rotation of wraparound with thickness at zero angle of attack in sub-supersonic flow.
  本文给出了亚、超音速弧翼的滚转及偏航阻尼力矩特性，并从理论上证明了零攻角时有厚度弧翼在亚、超音速绕流时正、反向滚转的必然性。
• When twin vertical fins are located at the wing surface the maximum lift coefficient could be increased obviously and the incidence range of yawing and rolling stability is extended.
  当双立尾分别移到机身外侧置于机翼上时，可以显著提高全机最大升力系数，同时使航向和滚转稳定的迎角范围大为扩展。
• Hydrodynamic Simulation and Analysis of Yawing of Bionic Robot Fish reciprocating power-driven tine harrow
  仿生机器鱼艏向摆动动力学仿真及分析动力驱动摆动式钉齿耙