1.
Dynamic response reliability analysis of airplane inner-flap mechanism
飞机内襟翼机构动态响应可靠性分析
2.
main foil flap hydraulic actuator
主翼襟翼液压执行机构
3.
camber changing flap
改变机翼弯度的襟翼
4.
The Design Study on the Kinematical Mechanism of Multi-Gap-Fowler-flap of Large-scale Cargo Airplane
大型运输机多缝富勒襟翼运动机构设计研究
5.
The aircraft would be made from composites that smoothed the airflow; the design has no slots or flaps.
飞机将采用表面光滑的复合材料制造以减少同气流的摩擦，并且不再附有翼缝和襟翼等结构。
6.
Research on Ground - effect - aircraft Flap Surcharge Relief Operating;
地效机襟翼超载自动释放操纵的研究
7.
Application of Gurney flap on certain target drone
Gurney襟翼在某型靶机上的应用
8.
Research of Calibration Technology on Angular Displacement for Elevator, Aileron and Flap of Airplane;
飞机升降舵、副翼和襟翼转角标定技术研究
9.
A variable control surface on the trailing edge of an aircraft wing, used primarily to increase lift or drag.
襟翼飞机后翼上最初用来增加上升力或拖力的可灵活控制的辅助翼
10.
leading-edge flap position indicator
前缘襟翼位置指示器
11.
trailing-edge flap position indicator
后缘襟翼位置指示器
12.
A brand new design for Monaco, with completely different main profile and flaps.
一个崭新的设计，完全不同于以往主体结构或是襟翼的外观。
13.
Design of Auto Tester for Aircraft Fairing Cone and Flap Based on ARINC 429 Bus
基于ARINC 429总线的飞机整流锥襟翼自动检查仪设计
14.
Design of Automatic Tester for Aircraft Fairing Cone and Flap Based on PC/104 Bus
基于PC/104总线的飞机整流锥襟翼自动检查仪设计
15.
airfoil control (system) combination
机翼和操纵机构组合
16.
The plane systems and functions are also recorded, along with information about engine thrust and the position of control surfaces (flaps and rudder).
同时，它也记录飞机的系统和运行情况，包括发动机的推力和操纵面位置（襟翼和方向舵）。
17.
A seagull hit the right wing tip, leading edge flap sustained minor damage.
右翼尖与一只海鸥相撞，前缘襟翼受到轻微损伤。
18.
Numerical Simulation of Usteady Flows over Gliding Flap of Multi-element Airfoils
多段翼型襟翼滑动非定常粘性流数值模拟