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
All-C/SiC composites body flap is gas-loaded intensely when the return of the space vehicle into Earth s atmosphere with high-supersonic.
针对全C/SiC复合材料机身襟翼再入过程中受到强烈的气动载荷作用的受力状况,进行了静力试验考核。
main foil flap hydraulic actuator
主翼襟翼液压执行机构
camber changing flap
改变机翼弯度的襟翼
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
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
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
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。
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。
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
Application of Gurney flap on certain target drone
Gurney襟翼在某型靶机上的应用
Design of Flapping Mechanism for a Micro Air Vehicle Based on Mathematical Morphology;
基于数学形态学的微扑翼飞行器翅翼机构设计
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。
Experiment on flow control using Gurney-flaps for a low-pressure turbine cascade
基于Gurney襟翼的低压涡轮叶栅流动控制实验
aileron: hinged part of the wing of an aircraft,used to control its balance while it is flying
副翼（飞机的机翼上控制飞行平衡的活动辅助翼）.
Calculation of the Aerodynamic Interaction between Rotor／Wing／Fuselage of Tilt-Rotor;
倾转旋翼飞行器旋翼/机翼/机身气动干扰计算
leading-edge flap position indicator
前缘襟翼位置指示器
trailing-edge flap position indicator
后缘襟翼位置指示器
A section of( wing trailing-edge) flap detached during flight probably due to material fatigue.
一段襟翼在飞行中掉落可能因材料疲乏。
We are trying to dump our fuel with gear down and full flaps.
我们试图将起落架放下和全襟翼进行放油。