wing tip

Air surveying and data analysis for dynamic response of missiles at swept-back wing tip

大后掠机翼翼尖导弹动力响应空测与数据分析

A seagull hit the right wing tip , leading edge flap sustained minor damage .

右翼尖与一只海鸥相撞，前缘襟翼受到轻微损伤。

The aviator warped a wing tip to regain balance .

飞行员使一机翼的端部翘起，以恢复平衡。

Investigators have released any suspected cause of the accident , bystanders say it appears a wing tip came off and there wasn 't explosion .

调查人员说明了可能引发事故的原因，目击者称，飞机的一侧机翼似乎折断，但并没有爆炸。

Based on computation and wind tunnel test , a rational aerodynamic configuration of sheared wing tip is posed , including optimum design of planform and airfoil , and the higher demands of increased lift and reduced drag at cruise and in climb are met .

在计算与风洞实验的基础上，提出了机翼剪切翼梢气动布局，对平面形状与翼型进行了优化设计，达到了巡航状态与爬升阶段较高的增升减阻要求。

Mechanism of lift augmentation and drag reduction on the sheared wing - tip

剪切翼梢增升减阻机理

This phenomenon is caused by interaction between the secondary separation vortices on the upper surface of the wing and the tip vortices .

这个现象的出现是由于翼尖涡和机翼上表面的二次分离涡相互作用，使翼尖涡发生失稳。

The presented method is limited to the combinations which consist of the bodies of finite or infinite lengths with curved axes and circular cross sections , and the wing of arbitrary planform with finite wing tip .

本文考虑的组合体其机身为有限或无限长，圆形截面，机翼前后机身轴线允许弯曲；

Baby hoatzins have a claw on the leading edge of each wing and another at the end of each wing tip .

幼麝雉在每个翅膀的边缘都有爪子，并且在翅膀顶部也会有爪子。

The last task is to test whether the scheme of optimized wing structure could satisfy the need of the overall design , including stability analysis , wing tip deformation displacement and strength requirement .

验证经优化后的机翼结构是否能满足总体设计要求，包括稳定性、翼梢变形位移和强度要求。