• CHORD - distance from leading to trailing edge of a wing.

    机翼前缘距离

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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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  • 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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  • We found we didn't need a flexible trailing edge concept, although this was one of the AFRL ideas for SensorCraft.

    我们发现需要可变形机翼后概念尽管AFRL传感飞行器设计概念之一。

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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 section of (wing trailing-edge) flap detached during flight probably due to material fatigue.

    襟翼飞行中掉落可能材料疲乏

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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)。

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  • 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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  • Operational abilities and excitation force characteristics of a new national trailing-edge fixed-vane excitation system (FVES) with a slotted rotating cylinder were verified by flight tests.

    针对一种研制旋转圆筒固定小翼激励系统,对其工作特性激励力特性进行了试飞验证

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  • The leading edge of the buffer has a mobility equal to or less than the surfactant, whereas the trailing edge has a mobility close to water.

    缓冲液前缘流度等于小于表面活性剂的流度,它的缘的流度接近于水的流度。

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  • The invention relates to a device for positioning the trailing edge of sheets in a blade folder.

    发明涉及用于定位优选组合式折页机中运动张的装置

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  • The improved blade according to claim 1 wherein a portion of the rovings extending from the loop towards the trailing edge comes to the surface of the filling towards the leading edge.

    改进刀片根据权利要求1其中一部无捻粗纱延长回路缘来表面填补迈向领先地位。

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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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  • The pressure roll is usually cooled both by internal circulating high velocity water and by placing a water-cooled aluminum roll against the trailing edge of the pressure roll as a heat sink.

    压力辊轴冷却通常通过个条件:使用内部高速循坏的流速,以及放置着压力辊轴的尾部作为散热器水冷辊轴。

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  • The aeroelastic analysis of a helicopter rotor blade with the controlled oscillating trailing edge flap is presented by building an aeroelastic model of the new concept rotor blade.

    通过建立受控振荡附翼概念旋翼气动弹性分析模型,研究了采用受控振荡附翼直升机旋翼气动弹性特性及其在降低旋翼振动载荷方面的有效性。

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  • Once the trailing edge vortex stays at the trailing edge the interaction of complex vortex structures occurs and no longer has a beneficial effect on the suction peak induced by the stall vortex.

    翼面上驻留时,各涡产生复杂相互干扰,对失速上翼面产生吸力不利影响

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  • Once the trailing edge vortex stays at the trailing edge the interaction of complex vortex structures occurs and no longer has a beneficial effect on the suction peak induced by the stall vortex.

    翼面上驻留时,各涡产生复杂相互干扰,对失速上翼面产生吸力不利影响

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