aerodynamic lift

英 [ˌeərəʊdaɪˈnæmɪk lɪft]

美 [ˌeroʊdaɪˈnæmɪk lɪft]

气动升力

英英释义

noun

• the component of the aerodynamic forces acting on an airfoil that opposes gravity
  Synonym:lift

双语例句

• The aerodynamic drag of the middle car varies within a small range, the aerodynamic lift of the rear car is greater than that of the front one;
  中间车阻力变化不大，尾车升力大于头车；
• To reduce aerodynamic drag and air pressure pulse of two trains meeting each other, and to increase aerodynamic lift, three streamline frontal shapes of high-speed maglev vehicle were designed according to the given section of train.
  为了降低列车交会空气压力波、减小空气阻力、使列车具有正的气动升力，根据给定的列车横断面，设计3种磁浮列车流线型头部外形。
• Then unstructured grids of two dimensional seat is constructed by the advancing front method, Euler equations are solved and aerodynamic damp, lift and moment coefficients of the seat are calculated at certain attack angles and Mach numbers.
  然后用推进阵面法建立了人-椅系统平面模型的非结构网格，并用Euler方程作为主控方程对某型座椅的气动阻力系数、升力系数和气动力矩系数进行了验证性计算；
• And the total aerodynamic lift of the three cars of the protruding longitudinal profile is greater than that of the concave.
  就整车升力而言，纵剖面轮廓线上凸的气动升力大于下凹的。
• The unique aim of aerodynamic designer is always to enhance lift coefficient and reduce drag coefficient.
  增升减阻一直是空气动力设计工作者追求的目标。
• The change rules of aerodynamic parameters including lift coefficient, drag coefficient and pitch moment coefficient have been analyzed when angle of attack and fuel flow rate is changed.
  考虑了不同飞行攻角、不同燃料流率下气动参数，包括升力系数、阻力系数和俯仰力矩系数的变化规律。
• The aerodynamic drag and lift of javelin increase with angle of attack.
  标枪的气动阻力、升力随迎角增加而增加。
• A Research on the Aerodynamic Characteristics of a Small Aspect Ratio, High Lift Fighter Configuration
  一种小展弦比高升力飞机的气动布局研究
• The RANS equations method for aerodynamic numerical simulation of a high lift configuration in 2D and 3D cases, the results of computation and their comparisons with experimental data are investigated in detail.
  深入研究了二维和三维高升力外形空气动力数值模拟计算的雷诺平均NS（RANS）方程方法、计算结果、以及它们和实验数据的比较。
• The main conclusion is that iced conductor can be galloping when the initial slop of curve of aerodynamic lift is negative and its absolute value is large enough;
  多分辨率曲线经研究发现：气动升力曲线初始斜率为负且其绝对值足够大时，结冰导线可能发生舞动；