aileron

Simulation of Static Test of Composite Aileron and Consistent Evaluation of Test and Analysis Results

复合材料副翼试验仿真及试验与分析一致性评估

The simulation study of the static test of composite aileron is carried out .

对复合材料副翼静力试验进行仿真研究。

Dynamic response of the aileron balance weight during landing impact

副翼配重的着陆冲击响应

And then the costs of two ailerons are estimated by using the developed code .

然后采用所开发的成本分析软件对两种方案的制造成本进行了评估。

Euler Solution of a 3D Wing - Body Configuration with Aileron

带副翼的翼身组合体绕流的Euler方程解

The method may be applied to differential aileron as well as plain aileron .

方法适用于简单副翼和差动副翼。

Leading - edge of Aileron with Variable Attached Weights of Flutter Analysis

前缘变配重颤振分析

Chimera Grid Calculation of 3D Viscous Flow over Wing with Aileron

带副翼三维机翼粘性绕流计算的嵌套网格方法

Aileron control and reconfiguration of flying wing aircraft A Kind of Composite Rotor Structural Optimization Design Model

飞翼布局飞行器副翼性能及重构分析一种复合材料旋翼结构优化设计模型

Finally the negative feedback effect of the aileron operation on the control parameters in the stable region is studied .

最后研究了副翼操纵反馈设计对操纵参数稳定域的影响。

The result shows that the system could used in the range of matching detection between ailerons to airfoil .

实践证明该系统可以应用于飞机副翼对机翼的吻合性检测。

You still have control over elevator and aileron but it can 't be over controlled .

你还可以控制电梯和副翼但不能超过控制。

I 've also carved one aileron and the fin fairing

我也刻一个副翼和鳍整流罩

The ailerons are moved in opposite senses to make the plane roll .

副翼向相反的方向转动就会使得飞机翻滚。

Still need to carve the ailerons , intakes and fin base .

仍然需要雕刻的副翼，摄入量和长须鲸的基础。

Airframe and powerplant Aileron control and reconfiguration of flying wing aircraft

飞行器构架和动力装置飞翼布局飞行器副翼性能及重构分析

This thesis proposed a technique using phase measuring profilometry to achieve inosculation between ailerons to airfoil detection .

为此本文提出了采用相位测量轮廓技术实现飞机副翼对机翼的吻合性检测。

The ailerons are movable sections along the rear edges of the wings .

副翼是机翼后缘的可动部分。

In the fuselage there are two independent hydraulic systems power the ailerons , rudder and other flight control surfaces .

机身内有控制副翼、舵面和其他翼面的双重独立液压操纵系统。

A lever used by a pilot to control the ailerons and elevators of an airplane .

飞行员用来控制飞机升降舵和副翼的杠杆。

The wings have controllable sections known as ailerons .

机翼上可操纵的部分叫做副翼。

Aileron control actuator leaked fluid .

副翼操纵作动筒漏油。

Analysis on Dutch Roll Modal of Unmanned Aerial Vehicle with the Limited Deadlocking of Single Aileron

无人机单副翼有限卡死时荷兰滚运动分析

A Euler method for solving the flow around a wing body configuration with deflection of control surface ( aileron ) is presented .

提出了一种求解带副翼偏转的翼身组合体绕流的Euler方程计算方法。

Vortex Lattice Image Method for Predicting the Aerodynamic Forces of Wing-body Combination with Aileron Down in Subsonic Flow

计算亚音速定常流中偏转副翼时机翼&机身组合体气动特性的涡格镜像法

The paper also describes a ground demonstration of a one channel primary flight control system and a flight demonstration of an aileron trim control system .

同时还介绍了一单通道主飞控系统的地面演示和一副翼配平控制系统的飞行演示。

It has plenty of aileron deflection and will rotate quite quickly in both directions while hovering .

飞机的副翼有很大的行程，所以飞机在悬停时，向左向右的滚转都很容易。

The computation of a wing-body combination with aileron

带副翼的翼身组合体的数值模拟

The ailerons on an airplane are hinged to the wing .

飞机的副翼是用铰链装在机翼上的。

The results indicate that the manufacturing cost of the composite aileron is lower than the metallic aileron because of using low-cost process and integrated design concept .

估算结果表明，复合材料副翼由于采用了低成本工艺与整体化的设计理念，其制造成本低于金属副翼。