1.
fuselage-wing-tail combination configuration
机身－机翼－尾翼组合体
2.
Tail-fin anchor
GB/T10829-1998尾翼锚
3.
APFSDS (Armor Piercing Fin Stabilized Discarding Sabot)
尾翼稳定脱壳穿甲弹
4.
Aerodynamics and Aerodynamic Heating Research for the Wing of Hypersonic Projectile;
高超声速弹箭尾翼（弹翼）的气动力与气动热研究
5.
The conventional tail must be at a negative angle of attack, and the Canard tail at a positive angle.
通常的尾翼必须处于负迎角，而鸭式尾翼则为正迎角。
6.
slow down by moving the tail sideways.
通过摇摆尾翼来减缓行进速度。
7.
a stabilizer that is part of the vertical tail structure of an airplane.
飞机的垂直尾翼部分的稳定器。
8.
The sideslipping airplane gives rise to a side force on the vertical tail.
侧滑的飞机在垂直尾翼上引起侧力。
9.
Analysis for Vertical Target Precision of APFSDS
尾翼稳定脱壳穿甲弹立靶密集度分析
10.
Wind Tunnel Experiments of Symmetric Discarding Sabot Disturbance of APFSDS Projectile
尾翼脱壳穿甲弹对称脱壳的风洞实验
11.
Empennage-Install Stabilizer and Vertical Fin.
尾翼－安装水平安定面、垂直安定面。
12.
A Numerical Wind Tunnel Study on Distance between Tail Wing and Rear Hood and Angle of Attack of Tail Wing of a Car Model Using CFD;
轿车尾翼间隙和攻角的数值风洞研究
13.
The Application Study of Affixed Cover in Forming Process of EFP with Fins
贴隔板法在尾翼EFP成型中的应用研究
14.
Numerical Simulation Study of Performance of Empennage Forming of Liner with Five Concave Arc Margins Cutted
五凹弧切边罩尾翼成形三维模拟研究
15.
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
16.
Experimental Research on EFP with Fins Formed by Four Detonating Points
四点起爆形成带尾翼EFP的试验研究
17.
The central body of an aircraft, to which the wings and tail assembly are attached and which accommodates the crew, passengers, and cargo.
机身可承载机务人员、乘客和货物的配有机翼和尾翼的飞机的主机
18.
The forces on an isolated tail are represented just like those on an isolated wing.
作用在单独尾翼上的力的表示方法正和单独机翼的情形一样。