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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

    • 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 sails, when correctly adjusted, will generate aerodynamic lift.
      帆时,正确地调整,将产生气动升力。
    • It's worth checking each item for obvious flaws
      有必要逐件检查一下是否有明显的瑕疵。
    • The aerodynamic/ stealthy integrated design is aim to obtain the maximum lift to drag ratio under constraints of stealthy performance through the adjustment of local shape de-sign variables. The task of the structure optimization is to minimize the structural weight by adjusting the size of structural components.
      气动/隐身一体化设计的任务是对局部外形设计变量进行优化,在满足隐身性能前提下,使升阻比最大;结构优化的任务是对结构尺寸进行优化,使结构重量最轻。
    • 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。
    • 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。
    • 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
    • Three seconds later, a stall-warning activated in the cockpit, indicating the jet was losing aerodynamic lift, Ms. Hersman said.
      赫斯曼说,三秒钟后,驾驶舱内的一个失速警告系统启动,显示飞机正在失去气动升力。
    • 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。
    • 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;