1.
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
2.
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。
3.
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
4.
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
5.
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。
6.
Experimental Investigation of Coaxial Rotor Wake
共轴式双旋翼尾迹形态的水洞实验研究
7.
3D simulation of over-turned explosively formed projectile(EFP) with star-shaped fins
带尾翼的翻转型爆炸成形弹丸的三维数值模拟
8.
Analysis on Wake Geometries and Flapping Responses for Rotor in Tilting Flight
倾转状态的旋翼尾迹形状和挥舞响应分析
9.
Experimental Study on Explosively Formed Projectiles with Fins and Numerical Simulation
贴隔板法形成尾翼型EFP的试验研究及数值模拟
10.
fuselage-wing-tail combination configuration
机身－机翼－尾翼组合体
11.
Tail-fin anchor
GB/T10829-1998尾翼锚
12.
double vee
双v形的, X形的
13.
The Influence of the Projectile Configuration on the Aerodynamic Characteristics of APFSDS for M=4～6,
马赫数4到6时弹丸外形对尾翼式脱壳穿甲弹气动力特性的影响
14.
APFSDS (Armor Piercing Fin Stabilized Discarding Sabot)
尾翼稳定脱壳穿甲弹
15.
On the Structural Style and Textual Function of the Overlap Form "V着V着";
“V着V着”结构形式及其语篇功能考察
16.
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
17.
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
18.
They form a wide letter @V@.
形成一个很宽的字母“v”。