1.
Effects of Leading-edge Vortex on Flutter Characteristics of High Sweep Angle Wing
大后掠翼前缘涡对其颤振特性的影响
2.
Leading edge structure design and analysis for bird impact
一种机翼前缘抗鸟撞结构设计与分析
3.
RCS of creeping wave for shadow region of wing leading edge
三维机翼前缘影区爬行波RCS研究
4.
Bird Impact on Aircraft Leading Edge Simulation with SPH and FEM Coupling Method
SPH和FEM耦合方法分析机翼前缘鸟撞的响应问题
5.
The receiver aircraft is fitted with a probe that extends out from the side of the fuselage or from the leading edge of the wing.
受油机装备有一个从机身一侧或者是机翼前缘伸出的探头。
6.
The tiles are backed by a high-temperature-resistant material on the nose and leading edges of the wings.
这些面砖敷贴在用耐高温材料制成的机头和机翼前缘。
7.
The outer rear edge of the wing of a bird, containing the primary feathers.
翼尖，前翼鸟翼的外后缘，包括初生毛
8.
leading-edge flap position indicator
前缘襟翼位置指示器
9.
a straight line connecting the leading and trailing edges of an airfoil.
连接机翼的前缘与后缘的直线.
10.
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。
11.
The effects of trailing edge jets on the vortex breakdown location over a delta wing
三角翼后缘喷流对前缘涡破裂位置的影响
12.
The front wing was hanging off and the right rear tyre was off the rim.
前翼掉了下来，右后轮胎濒临爆胎边缘。
13.
Adaptive feedback control of a nonlinear aeroelastic wing with leading-and trailing-edge surfaces
带前后缘控制面非线性翼段的自适应反馈控制
14.
Leading edge and trailing edge means the function of the dimmer.
飞机螺旋桨的前边缘和机翼后边缘是最能够反应调光器的功能的。
15.
The average length from the zygo-alveolar ridge to the pterygomaxillary junction was 26 mm, the average length from anterior nasal spine to the posterior nasal spine was 47 mm, and the angle between the piriform rim to the descending palatine canal and vertical section was 7 8'.
犁状孔边缘至翼腭管的距离平均为37mm; 前后鼻棘的距离为47mm;
16.
A handling party rushed forward and grabbed hold of special toggles on the trailing edges of the wings.
一群地勤人员冲向前去，抓住了机翼后缘上的特殊套环。
17.
The Application of Transonic Velocity Potential Equation with Higher Order Approximation for Computing the Pressure Distribution over the Blunt Leading-edge Airfoil
应用跨音速高级近似扰动速势方程计算钝前缘翼型的压力分布
18.
Numerical research on airfoil leading edge separation control using plasma actuator
应用等离子体进行翼型前缘分离控制的数值模拟研究