1.
To replace the relief valve disc, hold the upper guide fin and unscrew the diaphragm pressure plate.
要更换安全阀阀瓣，握住上部引导翼，旋下隔膜压力板上的螺丝。
2.
an aerodynamic missile
飞航式导弹, 有翼导弹
3.
aerodynamic characteristics of winged missile
有翼导弹空气动力特性
4.
Shape Optimization of Cruise Missile Based on the Concept of Telescopic Wing
伸缩弹翼巡航导弹气动外形优化研究
5.
Effect of Spinning Rate on Coupling Degree for Wing-deflection Rolling-missile
斜置尾翼导弹的转速对耦合度的影响
6.
This paper studied the wake improvement by stern fin and vortex generator numerically.
本文中利用数值计算讨论使用艉导流翼与涡流导流翼来改善艉迹流特性的可能性。
7.
Finally, it shows an application example of aerofoil missile.
最后给出了有翼导弹模块系统的应用实例。
8.
Experimental investigation on pressure distribution characteristics of wings of ×× missile at supersonic speeds and high angles of attack
××导弹翼面超声速大迎角压力分布特性试验研究
9.
The First Chinese Translator of Pushkin s Works --JI YI-hui and Pushkin;
普希金“初临中土”的向导———戢翼罝与普希金
10.
Sublimation investigation of artificial abduction crossflow stationary wave in swept wing
后掠翼人工诱导横流驻波的升华法研究
11.
Thermal-structural coupling analysis on wing short-range hypersonic missile
近程高超音速导弹弹翼热结构耦合分析
12.
INDUCED DRAG REDUCTION OPTIMIZATION STUDY USING MULTI-CONTROL SURFACES FOR ELASTIC WING
减小弹性机翼诱导阻力的多控制面优化研究
13.
Numerical Research of Rolling Characteristics on Canard Missiles by Distance between Fin and Wing
鸭式导弹舵翼面间距影响滚转的数值研究
14.
Analyzing Lateral and Directional Static Derivatives of Flying Wing Based on Conceptual Design
飞翼布局横航向气动导数的总体估算方法研究
15.
The Study of Induced Velocity Field and the Initial Trajectory of the Missile on the Condition of Coupled Rotor/Airframe Helicopter;
旋翼/机体耦合情况下的诱导速度场及对导弹初始弹道研究
16.
A fixed or movable airfoil used to stabilize an aircraft, a missile, or a projectile in flight.
安定翼，直尾翅用以稳定飞行中的飞机、导弹或发射体的固定式或活动式机翼
17.
Another new detail is on the turning vanes, which now feature a triangular, vertical fin (2).
另一项新细节在导流翼上，现在这片小翼变成一个三角形且垂直的鳍（2）。
18.
Resembling, containing, or composed of wings or alae.
翼状的，有翼的象翼或翼瓣的，包含翼的或翼瓣，由翼或翼瓣组成的