英语释义

• the rear edge of an airfoil

片语

trailing-edge control后缘操纵面

trailing-edge logic后沿逻辑

trailing-edge fold后缘褶皱

trailing brush edge后刷边

trailing-edge hole后缘孔

trailing-edge drag尾曳力

trailing-edge flap随边襟翼

trailing-edge tab[航]

英汉例句

• the flaperons have their own airfoil, and are hung below the wing trailing edge to supply them with fresh undisturbed air for maximum control effectiveness even at low speeds.

  襟副翼有自己的翼型，并挂在机翼后缘下方新鲜空气原状的速度控制在较低的最大效益，甚至他们与供应。

• aim to study the movement regularity of homogeneous soil landslide with known trailing edge and undetermined shear opening.

  目的研究均质土体滑坡（已知后缘裂缝位置，未知前缘剪出口位置）运动规律。

• 「if the results confirm our estimated performance, 」 said madsen, 「we will test the rubber trailing edge on a full-scale wind turbine within a few years.」

  madsen认为：「如果结果证实了我们估计的性能，几年内我们将在大型风机上测试橡胶尾缘。」

• in this thesis, the control law based on adaptive filter for smart rotor with actively controlled trailing edge flap is researched.

  本文主要研究基于自适应滤波的主动控制后缘附翼智能旋翼控制律设计问题。

• abstr: in the paper, reliability theory is applied in slope dumping damage analysis. the failure probability is determined according to trailing edge fracture development depth.

  文章摘要：本文将可靠度理论应用于边坡倾倒式破坏分析，根据后缘裂隙发育深度判定其破坏概率；

• the upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position.

  上表面在后缘装置处于收回位置时与机翼有一交汇点。

• in order to investigate the flow characteristics of cooling flow downstream of a turbine guide vane trailing edge slot , numerical methods of rng k-ε turbulent model were solved.

  通过rngk-ε湍流模型求解可压流的n-s方程，研究燃气轮机涡轮导向叶片尾缘劈缝出流冷气的流动情况。

• the work of this thesis is mainly about the design and test of an actuator for a smart rotor with the trailing edge configuration.

  本文对智能旋翼的研究主要是面向真实翼型的主动后缘襟翼智能旋翼驱动器模型设计和试验研究。

• in this paper, heat transfer and fluid flow in passage for trailing edge of turbine blade with pin-fin arrays is studied numerically.

  本文应用湍流模型对涡轮叶片尾缘针肋通道的换热与流动进行了二维数值模拟研究。

• and the viscous separation flow of wing-body trailing edge conjunction can be effectively simulated. therefore these algorithms are valuable for the engineering applications.

  计算结果与风洞实验的对比表明，文中所采用的数值方法可以有效的模拟翼身结合处粘性分离流动，具有一定的工程实用价值。

• the improved blade according to claim 1 wherein a portion of the rovings extending from the loop towards the trailing edge comes to the surface of the filling towards the leading edge.

  改进的刀片，根据权利要求1 ，其中一部份的无捻粗纱延长从回路对尾缘来表面填补迈向领先地位。

• as mentioned in the definitions section ks is the trailing edge thickness parameter.

  如上定义组是皇尾缘厚度参数。

• a turbine flow control technique using air ejection near blade trailing edge to achieve superior aerodynamic performance is proved numerically by cfd simulation.

  以某涡轮叶栅为研究对象，采用试验和数值模拟相结合的方式研究了涡轮叶片尾缘不同喷气形式对叶栅性能的影响。

• the leading and trailing edge is extracted based on the method of maximum radius error.

  采用基于最大半径误差的方法提取缘头。

• for example, the trailing edge of the wing is relatively shallow.

  例如，大翼后缘的厚度相对较薄。

• in one form, the universal dimmer begins each operation in the trailing edge mode and upon detection of an inductive load, switches to leading edge mode.

  于一个形式，通用减光器系开始各个操作于后缘模式，且当侦测一电感负载时而切换至前缘模式。

• in the forward fuselage a daimler-benz db 603 featured an annular-ring cowl, while exhaust stubs just aft of the trailing edge belied the position of the rear engine.

  在机身前部安置一台具有环形整流罩的戴姆勒-奔驰（daimler-benz）db603型发动机，同时排气管配置在尾部后发动机位置的后面。

• aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods.

  飞行器后缘设备，含运动路径非平行的设备，和有关方法。

• heat transfer in channel for trailing edge of turbine blade with pin-fin arrays is studied numerically.

  对涡轮叶片尾缘针肋通道的换热进行了数值模拟研究。

• the ejection from the symmetric slot blows away the vortex at the blade trailing edge and strengthens the mixing of the wake with the main flow.

  对开缝时，喷气引入吹除了附着在叶片尾缘的漩涡，并增强了尾迹与主流的掺混过程；

• each side of demon’s delta wing has one row of these slots in the upper part of its trailing edge and another on the lower part.

  「恶魔」无人机机翼上的每一边都在后缘上部装有一排这种狭槽，在后缘下部也装了一排。

• the movement occurs on the trailing edge of the pulse.

  移动是在脉沖的下降沿产生的。

• a numerical study has been performed for the condensing flows in a cascade, which has five different trailing edge shapes.

  本文对一个叶型五种出气边形状对应的凝结流动进行了比较，以初步揭示几何参数影响凝结流动的机理。

• to withstand the force of the oncoming air, a flight feather is shaped asymmetrically, the leading edge thin and stiff, the trailing edge long and flexible.

  为了抵御迎面而来的空气阻力，飞羽形成了非对称结构，其前缘又薄又硬，而后缘则修长且柔韧；