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

• 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。
• 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。
• Analysis the components of yawing system, and the process of a circular route of oil.
  对于偏航系统，分析了偏航系统的组成，液压控制偏航系统的油液循环路线的过程。
• 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。
• They were subject to violent yawing at low wind speeds.
  它们在低风速下会发生强烈的偏离。
• 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。
• The aerostatic bearings of minimum friction are used in two yawing measuring sets of the dynamometer. The power developed by turbine and the mechanical power lost in the turbocharger can be separately measured simultaneously.
  该测功机采用摩擦阻力最小的空气静压轴承作为两个测量机构的摆动轴承，能同时分别测出涡轮发出的功和涡轮增压器损失的机械功。
• By comparison and analysis of a large number of measured data, revealing the yawing motion of the FPSO is the main reason for this phenomenon.
  通过对大量的实测数据进行比较和分析，揭示了FPSO的艏摇运动是产生这种现象的主要原因。
• The range of yawing rate when turning left in hover is calculated, where the tail rotor might get into vortex ring.
  根据右侧飞试验结果，估算出样机悬停回转时尾桨处于涡环状态的偏航角速度范围；
• The yawing can apparently attenuate the angular displacement of both the tail and the attack angle of tail fin.
  艏摇的存在会明显的衰减尾柄主臂和尾鳍攻角的角位移。