deflections

英 [dɪˈflɛkʃənz]

美

n.  (尤指击中某物后)突然转向，偏斜，偏离
deflection的复数

柯林斯词典

• N-VAR 偏斜;偏转
  Thedeflectionof something means making it change direction.
  1. ...the deflection of light as it passes through the slits in the grating.
     光线通过光栅狭缝时的偏转
• (体育运动中球击中某物后的)转向，变向
  In sport, thedeflectionof a ball, kick, or shot is when the ball hits an object and then travels in a different direction.

双语例句

• In this paper, a new method to measure meshing composite deflections of loaded cylindrical involute helical gear by using high precision clinometer is presented.
  提出利用高精度测角仪测量齿轮副在啮合过程中不同啮合位置时轮齿受载综合变形的新方法。
• However, while some building codes provide methods for estimating shear wall deflections, these methods are not adequate for shear walls without hold-downs.
  尽管有些国家的建筑规范中已给出了估算木结构剪力墙侧向变形的方法，但这些方法并不适用于无抗倾覆锚固件木结构剪力墙。
• The deflections of the vertical happen to be known in this case ( see below).
  垂直偏斜碰巧在此例中有证明（看下图）。
• This renders the bearing like other self-aligning bearings, impervious to misalignments and shaft deflections.
  有这种装置的轴承就像自调整轴承，可以避免误差和轴倾斜。
• The deflections of throttle slices were analyzed and the equivalent relations of flux distribution were deduced according to the structure of self-designed hydro-pneumatic spring.
  根据自主研发阻尼可调油气弹簧的结构形式，分析了叠加节流阀片的挠曲变形量，给出系统流量分配的等效关系。
• The pace analyzes the current pre-arched calculation and installation method based on the relative deflections, and proposes a new absolute deflection method.
  本文在对现行的基于相对挠度的预拱度计算设置方法进行分析后，进而提出了新的绝对挠度法。
• Unsteady Transonic Flow Computation for a Wing with Control Surface Deflections by Euler Equations
  跨声速机翼操纵面非定常气动力Euler方程计算
• The deflections of the blades under different wind speeds and different rotating time were given to validate the reliability of the model presented herein.
  研究结果对风力机叶片的振动特性和疲劳寿命预测以及高性能叶片的设计有理论指导意义。
• So the deflections of concrete beams prestressed with bonded FRP tendons are expected to be larger than those of the steel bars cases.
  国内外已有试验研究表明，有粘结预应力FRP筋混凝土梁的破坏模式包括界限破坏、受压破坏与受拉破坏三种。
• When aerodynamic solution and structural deflections are both converged, the aerodynamic characteristic of the elastic wing is obtained.
  将非线性气动力与结构线化机翼弹性变形耦合迭代求解。