1.
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
2.
an aerodynamic missile
飞航式导弹, 有翼导弹
3.
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
4.
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
5.
aerodynamic characteristics of winged missile
有翼导弹空气动力特性
6.
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
7.
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
8.
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
9.
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
10.
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。
11.
Elastic buckling of web restrained by flanges in I-section members
考虑翼缘约束的工字形截面腹板的弹性屈曲
12.
In contrast to the aerodynamic winged vehicle, a true ballistic missile is controlled for only a few minutes at the start of its flight.
与空气动力有翼导弹大不相同，一枚真正的弹道导弹只在起飞的几分钟内受人们控制。
13.
a missile that flies level with the ground
贴着地面飞行的导弹
14.
Several Problems of Surface-to-Air Missile System Derived from Air-to-Air Missile
空空导弹移植为面空导弹需要考虑的几个问题
15.
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
16.
Integrated Modeling Method Including Aerodynamics and Radar Stealth of Winged Missile Conceptual Design;
有翼导弹概念设计中的气动/隐身一体化建模研究
17.
Experimental Study on Decelerating and Spinning Characteristics of an Asymmetric Two-wing Projectile
一种非对称双翼结构弹丸减速导旋特性试验研究
18.
Numerical Simulation of Cruciform Missile at High Angle of Attack Based on N-S Equation
基于N-S方程的十字翼大攻角导弹绕流数值模拟