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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

    • At the rear, a carbon fibre'sharks tooth'rear vortex generator helps to reduce aerodynamic lift.
      在后方,一个碳纤维的鲨鱼的牙齿的后方能降低空气涡流发生器的电梯。
    • 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
    • Turbine aerodynamic mortar insurance agency is a mechanical fuze in a key insurance and lift the insurance institutions.
      涡轮式空气动力保险机构是迫击炮弹机械触发引信中一道关键的保险与解除保险机构。
    • Results show that oscillating excitation adding at the surface of the airfoil can improve aerodynamic performance thus increase lift force of airfoil.
      结果表明在深失速条件下,翼型头部附加的振荡扰流在一定的频率和振幅时能够显著改善翼型的气动性能,提高翼型的升力。
    • It is shown that aerodynamic force coefficients of vehicle-bridge coupled system, consisting of lift coefficient, drag coefficient and moment coefficient, significantly change in different wind directions.
      计算过程中,在不同风向角工况下,车桥耦合体系的气动力系数,包括升力系数、阻力系数和倾覆力矩系数,都发生了明显的增大。
    • 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。
    • The investigation illustrated that the aerodynamic lift and pitching moment of wing can be predicted accurately by CFD based on RANS approach with comparison to model tests.
      结果表明与模型试验数据相比,基于RANS方程的CFD方法能够准确预报机翼的气动升力和力矩。
    • Rear spoiler not only makes the automobile the aerodynamic lift to reduce, but also can effectively reduce the resistance and availably lower the resistance that car be subjected to.
      后扰流板不仅可以使汽车的气动升力得到降低,还能有效地降低汽车所受阻力。
    • An experimental research is completed in a 3 4 m × 2 4 m wind tunnel, the purpose is to determine the aerodynamic characteristics of a ducted fan system, especially the lift and drag of the duct in the complex airflow.
      为了研究涵道风扇系统的气动特性,尤其是在复杂流场中涵道本身的升阻特性,在3.4m×2.4m开口风洞中对涵道风扇进行了吹风试验。