最大厚度位置的英文

• maximum thickness position
• thickness distance

• "最大"英文翻译    maximum
• "厚度"英文翻译    thickness; land
• "位置"英文翻译    seat; place; location; site
• "最大厚度" 英文翻译 :    maximum gauge; maximum thickness
• "最大厚度线" 英文翻译 :    maximum thickness line
• "工件最大厚度" 英文翻译 :    maximum thickness of work; thickness of work
• "胶质层最大厚度" 英文翻译 :    maximum thickness of gelatine layer; maximum thickness of plastic layer
• "翼型最大厚度点" 英文翻译 :    crest of airfoil
• "中空玻璃最大厚度" 英文翻译 :    max.thinkness of insulating glass
• "最大厚度或直径" 英文翻译 :    maximum gage; maximum gauge
• "大厚度" 英文翻译 :    heavy section
• "工件锯割或锉削最大厚度" 英文翻译 :    maximum sawing or filling thickness of work; maximumsawingorfillingthicknessofwork
• "零速度位置" 英文翻译 :    zero eed position; zero speed position
• "后跟高度位置" 英文翻译 :    back seam tack
• "后踵高度位置" 英文翻译 :    back seam tack
• "相对高度位置" 英文翻译 :    relative altitude position
• "大开度位置的襟翼" 英文翻译 :    highly-deflected flap
• "阀的很小开度位置" 英文翻译 :    cracked position
• "高度位置指示器" 英文翻译 :    height position indicator; height-position indicator
• "很小的开度位置" 英文翻译 :    cracked position
• "角度位置传感器" 英文翻译 :    angular position sensor
• "角度位置式密度传感器" 英文翻译 :    angular position type density sensor
• "头盔角度位置感测器" 英文翻译 :    helmet-angle position sensor (haps)
• "陀螺球高度位置指示表" 英文翻译 :    height indicator of gyrosphere
• "陀螺球高度位置指示器" 英文翻译 :    height indicator of gyrosphere

• 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