Control Surface: Aileron, Elevator and Rudder.
控制舵面：副翼，升降，方向。
The rudder is a control surface that steers and stabilises the boat.
舵是控制表面，公牛和稳定的船。
On the right display, I have the control surface position display pulled up.
在右边的显示器上，我打开了控制面位置的显示界面。
The aerodynamic forces on any control surface produce a moment about the hinge.
在任何操纵面上的空气动力均产生围绕其铰链轴的力矩。
The control surface on the tailplane of an aircraft that makes it ascend or descend.
能够控制升降的装在飞机横尾翼上的操纵面。注意，注意力集中。
A new type of rotary actuator for driving the wing control surface has been studied.
研究出一种翼面驱动用旋转作动器。
The control surface deflection is modeled by using an equivalent body velocity approach.
操纵面偏转用物面当量法向速度模拟。
The wing has a two-spar structure and an active control surface for gust response alleviation.
该机翼具有双梁式结构和一个用于阵风响应减缓的主动控制面。
Remember, you don't have direct control over the amount or direction of control surface deflection.
记住，你并没有直接操作控制面偏转的方向和大小。
Applicable range of this model and way for improving control surface efficiency have been pointed out.
指出数学模型的适用范围和改善操纵面效率的途径。
CONTROL SURFACE, Moveable panels on wings and tail for movement of airplane on pitch, roll and yaw axes.
操纵面，机翼和机尾上的可动面板，用以操纵飞机俯仰，坡度，和偏航运动。
The TAB moves in an opposite direction to the control surface for assisting movement of the control surface.
随动补偿片的动作方向与操纵面相反，以帮助操纵面运动，减小操纵力。
Most compositions, such as scene system, flight system, flight's sound and control surface are all simulated.
模拟了飞机的主要系统：飞行系统、视景系统、仪表系统和音响系统。
BALANCE TAB, a small hinged moveable part on the trailing edge of a control surface (aileron, elevator, rudder).
随动补偿片，铰接在操纵面后缘(副翼，方向舵，升降舵)的可动部。
This paper presents a new approach to determining the moments of inertia of the control surface or tab about its hinge line.
本文提供了一种试验测定操纵面或调整片绕自身铰链轴线的转动惯量的新方法。
A numerical method is presented for predicting unsteady transonic aerodynamic flow about aircraft wings with control surface.
本文介绍一种带操纵面机翼的非定常跨声速流的有限差分计算方法。
Based on different forms of hinge points and rocker - arms, four local models of control surface linkage forms were proposed.
根据舵面悬挂点与摇臂操纵形式的不同，提出了四种连接方式的局部模型。
Numerical results show that the present method is effective for solving the flow around a wing with control surface deflection.
数值算例表明该方法是求解带操纵面偏转的机翼绕流的有效方法。
In this paper, employing rigorous variational calculus, equations of control surface at maximum thrust nozzle exit are derived.
本文用严格的变分法导出了最大推力喷管出口控制面方程。
Numerical results show that the present method is effective one for solving the flow around wing with control surface deflection.
数值算例表明本方法是求解带操纵面偏转的机翼绕流的有效方法。
A movable control surface, usually attached to the horizontal stabilizer of an aircraft, that is used to produce motion up or down.
升降舵一个可动控制台，通常安装在飞机的尾翼上，用来操纵飞机。
An optimization method is used to obtain deflection Angle of control surface and the aerodynamic efficiency of airfoil is calculated.
用数值优化方法取得自适应翼型最优的舵面偏角，并计算其气动特性。
Numerical results show that present method is an effective one for solving the flow around wing body configuration with control surface deflection.
数值算例表明本文方法是求解带操纵面偏转的翼身组合体绕流的有效方法。
Numerical results show that the present method is effective one for solving the flow around a wing body combination with control surface deflection.
数值算例表明该方法是求解带操纵面偏转的翼身组合体绕流的有效方法。
As for the problem of surface roughness measure of deep hole in measure field, developed a kind of portable micro-control surface roughness instrument.
针对测量领域深孔表面粗糙度测量存在的问题，研制了一种便携式微控表面粗糙度检测仪。
As for the problem of surface roughness measure of deep hole in measure field, developed a kind of portable micro-control surface roughness instrument.
针对测量领域深孔表面粗糙度测量存在的问题，研制了一种便携式微控表面粗糙度检测仪。
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