wingtip

n.  翼尖;翼稍

复数:wingtips

BNC.37963 / COCA.24682



双语例句

  1. The kite is then landed on the opposite wingtip and held in that position for at least two seconds.
    风筝然后以另一个剑尾(脚)着陆,并保持这个姿势至少2秒钟。
  2. Touched him with a wingtip!
    只用翼梢碰他一下!
  3. Shape Parameter Optimization for Wing and Wingtip Based on RBF
    基于径向基函数的机翼和翼梢小翼外形优化
  4. A single wingtip feather, he found, moved a fraction of an inch, gives a smooth sweeping curve at tremendous speed.
    他发现,把翼消的一根羽毛转动那么一丝丝,就可以在高速下平平稳稳地来个急转弯。
  5. The secondary structures, which support aerodynamic fairings or skins, flight control surfaces and control mechanisms, consist of the leading edge, trailing edge, and wingtip.
    次要结构由机翼前缘,后缘和翼尖构成,主要用来减小空气阻力,支撑蒙皮,协助飞行操纵面和操纵机构。
  6. Wingtip Dual inflation zippers: To inflate your kite with effortless input, for a safer and easier launch.
    翼梢双重通货膨胀拉链:膨胀您的风筝以不出力的输入,为更加安全和更加容易的发射。
  7. His wingtip shoes crunch on gravel. Loose bullets scatter to the ground. The bourbon bottle drops and shatters.
    他的翼尖鞋轧在砾石路上,任子弹散落在地,波旁酒瓶也摔到地上,碎了。
  8. Shown is the curved wingtip of the787 Dreamliner.
    显示的是波音787梦想飞机翼尖弯曲。
  9. They'd cruise so close that I could sense the leader's wingtip only centimetres from my cheek.
    它们离我很近,我能感到那只领头雁的翅膀尖距我面颊只有几厘米。
  10. The insignia was visible on the wingtip.
    翼梢上的徽记清晰可见。
  11. He did several sweeping low-level banked passes as well as his trademark aerobatic routine complete with smoke from the wingtip canisters.
    他没有几个席卷低水平库通行证以及他例行商标特技完成烟雾滤毒罐的翼梢。
  12. Touched him with a wingtip! Brought him to life! The Son of the Great Gull!
    只用翼梢碰他一下!把他救活了!真是鸥神之子!
  13. The aircraft also has six ( four under-wing and two wingtip) pylons to carry various air-to-air and air-to-ground weapons.
    飞机也有六(四个在机翼下和二个在翼尖)挂架携带各种不同的空对空和空对地武器。
  14. Even at the margins, the collisions were devastating: the wingtip of the second plane grazed the78th floor sky lobby in the south tower, instantly killing dozens of people waiting for elevators.
    就连大楼的边边角角也遭到了彻底的破坏。第二架飞机的翼尖擦过了南楼78层,正在等电梯的几十人当即死亡。
  15. In order to provide security assurance for airplane ground movement, wingtip tracking is put forward which is based on video image processing and analysis techniques.
    研究基于视频图像分析与定位的飞机翼尖跟踪技术,为飞机地面移动提供安全保障。
  16. A Method for Determining the Requirements of Wingtip Deflection and Wing Section Rigidity of Flight Vehicles
    确定飞行器翼尖挠度和翼面刚度要求的方法
  17. Image method ideal vortex model is used for the analysis of how ground effect impacts wingtip vortex and airflow downwash angle.
    采用镜像法理想涡模型分析了地面效应对翼尖涡位置和气流下洗角的影响;
  18. Characteristics of tailless aircraft wingtip stalling, including common and unique characteristics compared with other configurations, are analyzed with emphasis placed on the effect of wingtip stalling on flying qualities of tailless aircraft.
    首先分析了无尾飞机翼尖失速的特点,包括与其他布局形式共有的和自身特有的特点,重点是翼尖失速对无尾飞机飞行品质的影响。
  19. The structure of wingtip vortex and the affection of tap on wingtip vortex is investigated in this paper.
    本文的研究目的是弄清机翼翼梢涡的结构及安装翼梢扰流片对翼梢涡的影响。
  20. The influence of sweep angle and taper ratio on the characteristics of wingtip stalling is discussed.
    讨论了后掠角和尖削比这两个机翼外形参数对翼尖失速特性的影响。
  21. Study of Method of Design of Winglet on Wingtip of Certain Type of Plane Based on Perpendicular Design
    基于正交设计的某型飞机翼尖小翼优化设计方法研究
  22. Analysis of Wingtip Stalling for Tailless Aircraft
    无尾飞机翼尖失速问题研究
  23. This paper presents the constraint condition of wingtip deflection and the conversion formulas of wing section rigidity on the basis of combining theory with practice.
    本文基于半理论半经验的方法,为翼面提出了翼尖挠度限制条件和翼面刚度换算公式。
  24. The wingtip deformation is also satisfied with the distortion.
    通过有限元分析,翼尖扰度也满足变形要求。
  25. The effects of wingtip's speed 、 angle of attack and the airfoil shape on wing's aerodynamic characteristics are presented.
    研究了桨尖马赫数、机翼桨距角及机翼剖面的不同外形对旋翼气动特性的影响。
  26. Then, the effective wind components and gradients are introduced into the standard six-DOF nonlinear aircraft kinematics equations and dynamics equations to determine the effects on the follower's dynamics induced by the wingtip vortex of leader aircraft.
    然后就可以将有效风分量与风梯度引入到标准的六自由度飞机运动学和动力学非线性方程组中计算出长机翼尖涡对僚机动力学的影响。
  27. The difference between point wingtip and roundness wingtip for the flight performance of the aves is so obvious.
    尖形翼尖与圆形翼尖的形状差异对鸟类的飞行能力差异明显。
  28. Contrastive analyses indicate that the winglet and C-type wingtip produce remarkable adverse effects on flutter characteristics of transport wing.
    翼梢小翼和C型翼梢对基本机翼的颤振特性产生了明显不利影响。
  29. Wingtip shape has enormous implications for the flight of the aves.
    翼尖形状对于鸟类飞行的能力影响很大。
  30. Also the aerodynamic and mass effects of wingtip devices are identified separately by way of setting virtual mass.
    分析中还采用虚拟质量方法分离了翼梢装置质量和气动力的作用。