释义 |
trailing edge ˌtreɪlɪŋˈedʒ 短语⁸⁴³²⁰⁺⁸ 基本英英例句例句 n.飞机的机翼后缘
Noun: the rear edge of an airfoilA variable control surface on thetrailing edgeof an aircraft wing, used primarily to increase lift or drag.襟翼飞机后翼上最初用来增加上升力或拖力的可灵活控制的辅助翼 For recognition, the front or trailing edge of projection of binary image on horizontal axis basically shows linear shape, so least square theory is applied in tilt correction. 识别过程中,数码管二值化后的图像在水平轴上的投影,其上升沿或下降沿基本呈现直线的形状,尝试把最小二乘法应用于倾斜校正。 cnki The leading edge of the buffer has a mobility equal to or less than the surfactant, whereas the trailing edge has a mobility close to water. 流度缓冲液的前缘的流度等于或小于表面活性剂的流度,而它的后缘的流度接近于水的流度。 www.infopetro.com.cn The pressure roll is usually cooled both by internal circulating high velocity water and by placing a water-cooled aluminum roll against the trailing edge of the pressure roll as a heat sink. 压力辊轴的冷却通常是通过两个条件:使用内部高速循坏的水流速,以及放置一个对着压力辊轴的尾部作为散热器的水冷却铝辊轴。 blog.sina.com.cn The trailing edge of the second pulse, therefore, also acts as an event horizon. 因此,第二个脉冲的后缘地带也发挥了视界的作用。 ecocn Thus the solution of unsteady problem in the time domain is transformed into the solution at each harmonic order. The Kutta condition of equal pressure at the trailing edge is employed. 所有的时域参数通过傅里叶级数展开转化为频域参数,使得在时间域内的求解转化为每一谐调阶上的求解。 ilib 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。 cnki 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。 cnki Philip John, the technical director of the project, says the version used on Demon has the compressed air entering a single chamber within a wing’s trailing edge. 菲利普•约翰 Philip John是该项目的技术负责人,他说“恶魔”无人机是将压缩空气导入机翼后缘的一个气腔内。 ecocn That has some signature implications, with what looks like an almost unswept trailing edge, because edges scatter forward and backwards. 这里有些特征性暗示,看上去机翼后缘几乎没有清理过,因为有些翼缘前后散开着。 bbs The light stall is characterized by the trailing edge separation and the influence of separation bubble is restricted in the rear part on the airfoil. 计算结果显示:轻失速主要是由于后缘分离引起,分离涡的影响范围主要是在后缘附近。 cnki |