中英
aerofoil
/ ˈeərəfɔɪl /
/ ˈerəfɔɪl /
  • 简明
  • 柯林斯
  • n.[航] 机翼;机翼剖面
  • 网络释义
  • 专业释义
  • 英英释义
  • 1

    [航] 翼面

    ... aero filter 空气过滤器 aerofoil 翼型,机翼型;翼面;机翼 aerofoil blading 翼面叶 ...

  • 2

     翼型

    ... airfoil section 翼剖面,翼型... biconvex airfoil 双凸翼 aerofoil 翼型 ...

  • 3

     气翼

    ... 空气动力学 aerodynamics 气翼 aerofoil 翼形断面 aerofoil section ...

短语
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  • 双语例句
  • 1
    Transformative problem of aerofoil impeller is put forward.
    提出了机翼型叶轮的改造问题。
  • 2
    The rotor blades work like the wings of an aeroplane, with an aerofoil shape providing lift.
    旋转叶片的工作原理类似飞机的两翼,运用机翼的形状提供上升力。
  • 3
    The blades have an aerofoil shape and provide lift when passing through air, like the wings of an aeroplane.
    这些叶片拥有机翼的剖面形状,它们就像普通飞机的机翼那样,通过划过空气来产生升力。
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  • 同近义词
  • 词源
  • n.

    [航]机翼;机翼剖面

    airfoil

  • 百科
  • Aerofoil

    An airfoil (in American English) or aerofoil (in British English) is the shape of a wing or blade (of a propeller, rotor, or turbine) or sail as seen in cross-section.An airfoil-shaped body moved through a fluid produces an aerodynamic force. The component of this force perpendicular to the direction of motion is called lift. The component parallel to the direction of motion is called drag. Subsonic flight airfoils have a characteristic shape with a rounded leading edge, followed by a sharp trailing edge, often with asymmetric curvature of upper and lower surfaces. Foils of similar function designed with water as the working fluid are called hydrofoils.The lift on an airfoil is primarily the result of its angle of attack and shape. When oriented at a suitable angle, the airfoil deflects the oncoming air, resulting in a force on the airfoil in the direction opposite to the deflection. This force is known as aerodynamic force and can be resolved into two components: lift and drag. Most foil shapes require a positive angle of attack to generate lift, but cambered airfoils can generate lift at zero angle of attack. This "turning" of the air in the vicinity of the airfoil creates curved streamlines which results in lower pressure on one side and higher pressure on the other. This pressure difference is accompanied by a velocity difference, via Bernoulli's principle, so the resulting flowfield about the airfoil has a higher average velocity on the upper surface than on the lower surface. The lift force can be related directly to the average top/bottom velocity difference without computing the pressure by using the concept of circulation and the Kutta-Joukowski theorem.

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