1.
camber changing flap
改变机翼弯度的襟翼
2.
main foil flap hydraulic actuator
主翼襟翼液压执行机构
3.
Development of a morphing wing with adaptive capability
采用智能材料的变弯扭机翼实验研究
4.
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
5.
Application of Gurney flap on certain target drone
Gurney襟翼在某型靶机上的应用
6.
Effect of Aerofoil Camber on Airfoil Aerodynamic Performance
风力机的翼型弯度对风力机翼型气动性能的影响
7.
A single flap replaces the previous double design and the additional winglets over the main profile have increased in length, almost reaching the side of the nosecone.
单襟翼取代了原本双襟翼的设计，同时主体上方额外的翼端帆长度也增加，现在几乎要碰到鼻锥。
8.
Influence of chordwise bending stiffness on aeroelastic characteristics of flexible high-aspect-ratio wing
水平弯曲刚度对大展弦比机翼颤振的影响
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.
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
11.
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
12.
A variant of the swept-back wing is the delta wing.
后掠翼的变型是三角翼。
13.
Corneal topographic changes after excision of pterygia
翼状胬肉切除术后角膜地形图及散光度的改变
14.
For straight-winged tailless airplanes, only the negative camber satisfies the conditions for flight.
对直机翼无尾飞机，只有负弯度才满足飞行条件。
15.
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。
16.
Design and installation of 4000 DWT multi-purpose carrier flapped rudder
4000DWT多用途船襟翼舵的设计与安装
17.
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
18.
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