• AILERON, a hinged moveable part on the trailing edge of each wing for airplane roll (wing up and wing down) control.

    副翼每个机翼可动部件用于控制飞机滚转(机翼向上向下)。

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  • The flaperons have their own airfoil, and are hung below the wing trailing edge to supply them with fresh undisturbed air for maximum control effectiveness even at low speeds.

    副翼自己翼型机翼下方新鲜空气原状速度控制较低最大效益甚至他们供应

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  • BALANCE TAB, a small hinged moveable part on the trailing edge of a control surface (aileron, elevator, rudder).

    补偿片,铰接操纵缘(副翼,方向舵,升降舵)可动部。

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  • ELEVATOR, a hinged moveable part on the trailing edge of the horizontal stabilizer for airplane pitch (nose up and nose down) control.

    升降舵水平安定面可动部件。用以操纵飞机俯仰运动(机头)。

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  • A hinged moveable part on the trailing edge of each wing for airplane roll (wing up and wing down) control.

    每个机翼可动部件用于控制飞机滚转(机翼向上向下)。

    youdao

  • Looking at that in the lab, it becomes a function of airfoil shape, and also of the flow control technologies you use to enhance the laminar flow with conformal trailing edge surfaces.

    实验室研究表明,已经成了机翼一项功能也是通过适形机翼后表面增强层流控制技术的功能。

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  • In this thesis, the control law based on adaptive filter for Smart Rotor with actively controlled trailing edge flap is researched.

    本文主要研究基于自适应滤波主动控制附翼智能旋翼控制设计问题。

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  • In addition, the trailing edge jets may weaken or even eliminate the mixing phenomenon of the leading edge vortex, which is in advantage of the flight control of aircraft.

    另外喷流可以减弱乃至消除前缘混掺现象发生,进而有利于飞行器的操纵

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  • This paper gives a brief description of the whole process of the low-speed wind tunnel test for active flutter suppression of a two-dimensional wing model with trailing edge control surface.

    本文简要地阐述了具有控制面的二元机翼模型主动颤振抑制低速风洞试验全过程

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  • This paper aims at presenting an investigation into aerodynamics and control reversal characteristics of adaptive wings with seamless, variable camber, flexible trailing edge.

    建立了带柔性后缘自适应机翼模型带刚性偏转后传统机翼模型,从升阻特性和力矩特性以及操纵效率对它们进行了比较研究

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  • The secondary structures, which support aerodynamic fairings or skins, flight control surfaces and control mechanisms, consist of the leading edge, trailing edge, and wingtip.

    次要结构由机翼前缘,后缘构成主要用来减小空气阻力,支撑蒙皮,协助飞行操纵和操纵机构

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  • The secondary structures, which support aerodynamic fairings or skins, flight control surfaces and control mechanisms, consist of the leading edge, trailing edge, and wingtip.

    次要结构由机翼前缘,后缘构成主要用来减小空气阻力,支撑蒙皮,协助飞行操纵和操纵机构

    youdao

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