机翼后缘的英文

• trailing edge

• "机翼"英文翻译    wings of an aeroplane side; ...
• "后缘"英文翻译    trailing edge
• "机翼后缘增升装置" 英文翻译 :    wing trailing-edge device
• "尖翼后缘" 英文翻译 :    tapered trailing
• "机翼后掠角" 英文翻译 :    wing sweep setting; wing-sweep angle
• "机翼后的气流" 英文翻译 :    downstream of wing
• "机翼后的下洗" 英文翻译 :    downwash behind wing
• "机翼后掠角变化" 英文翻译 :    wing sweep movement
• "自动改变的机翼后掠角" 英文翻译 :    automatic variable wing sweep
• "后缘" 英文翻译 :    trailing edge◇后缘襟翼 trailing edge flap
• "机翼" 英文翻译 :    [航空] wing; wing unit; aerofoil; airfoil
• "前翼后掠角" 英文翻译 :    forewing sweep
• "外翼后掠角" 英文翻译 :    outboard wing sweep; sweep of outer panels
• "尾翼后掠角" 英文翻译 :    sweep of the tail
• "陡后缘" 英文翻译 :    abrupt trailing edge
• "钝后缘" 英文翻译 :    blunt trailing edge
• "帆后缘" 英文翻译 :    after leech; leech (or leach)
• "后缘板" 英文翻译 :    posterior marginal shield
• "后缘层" 英文翻译 :    posterior border layer
• "后缘的" 英文翻译 :    trailing
• "后缘脊" 英文翻译 :    posterior edge
• "后缘角" 英文翻译 :    angle of trail; trailing-edge angle
• "后缘孔" 英文翻译 :    trailing-edge hole
• "后缘流" 英文翻译 :    trailing-edge flow
• "后缘脉" 英文翻译 :    postal vein

• The ailerons are movable sections along the rear edges of the wings .
  副翼是机翼后缘的可动部分。
• 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。
• Stiff struts and ribs meant that wings were too rigid to flex much torsionally , so builders installed ailerons ? flaps located on the outer , trailing - edge portions of wings
  难以弯曲的支柱和翼肋，使得机翼太过刚硬，同时也限制了扭转幅度，因此工程师加上了副翼，也就是位于机翼后缘外侧的襟翼。
• Abstract : the effects of airfoil geometric parameters on wing " s spacial and polarized scattering characteristics have been systematically revealed . the results of the study indicated that the calculating value of diffraction from trailing edge by using the formula of the straight wedge is very far from experimental results for vertical polarization , and the contribution of thickness of the trailing edge to scattering must be considered in the calculation . the scattering peak of leading edge depends only on radius of airfoil for horizontal polarization . but for vertical polarization , it depends on maximum thickness and the location of maximum thickness . engineering formulas for evaluating all scattering peaks were given in the paper . it is important for the design of low - rcs wing
  文摘:系统地揭示了翼形几何参数对机翼的空间散射特性、极化散射特性的影响规律.研究发现，在垂直极化状态下用理论尖劈公式计算机翼后缘绕射的计算结果与实验结果相差甚远.提出在垂直极化状态下机翼后缘绕射的计算必须将后缘厚度考虑在内的见解.对于水平极化，前缘散射波峰只与前缘半径有关；而对于垂直极化，前缘散射波峰与翼形最大厚度以及最大厚度位置有关.给出前后缘散射波峰的工程估算公式，为低雷达散射截面( rcs )机翼设计提供依据