1.
Lateral Performance Analysis and Stability Augmentation Control of Tailless UAV
无尾翼无人机横侧向分析与增稳控制设计
2.
Flow Control Technique for Forward-swept Wing Blended Body Tailless Configuration
前掠翼融合体无尾布局流动控制技术
3.
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。
4.
Numerical Simulation on Lengthways Aerodynamic Characteristics of UAV with Vee Tail under Jet Flow Influence
V形尾翼无人机喷流对纵向气动影响数值模拟
5.
fuselage-wing-tail combination configuration
机身－机翼－尾翼组合体
6.
Tail-fin anchor
GB/T10829-1998尾翼锚
7.
APFSDS (Armor Piercing Fin Stabilized Discarding Sabot)
尾翼稳定脱壳穿甲弹
8.
"King's Indian, Fianchetto without c4"
王翼印度,侧翼象无c4
9.
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
10.
Maneuver Load Optimal Distribution Between Canard and Horizontal Tail of Three-surface Aircraft
三翼面飞机前翼和平尾机动载荷优化配置
11.
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。
12.
The wings and tails help the aircraft take off,
机翼和机尾帮助飞机起飞，
13.
slow down by moving the tail sideways.
通过摇摆尾翼来减缓行进速度。
14.
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。
15.
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。
16.
long-billed warm-water seabird with wide wingspan and forked tail.
温暖水域长嘴的海鸟，翼幅宽、尾叉形。
17.
Eurasian pigeon with white patches on wings and neck.
欧亚大陆翼和尾上有白色斑点的鸽子。
18.
the vertical airfoil in the tail assembly of an aircraft.
飞机尾部组成部分的垂直机翼。