掠角的英文

• grazing angle
• sweeangle

• "角"英文翻译    role; part; character
• "后掠角" 英文翻译 :    angle of sweep back; angle of sweepback; backswept; backward sweep; sweep angle; sweep back angle; sweepback angle; sweepback swept-back angle; swept back wing
• "前掠角" 英文翻译 :    sweepforward
• "大后掠角" 英文翻译 :    sharp sweep angle
• "大后掠角的" 英文翻译 :    adcutely swept
• "改变后掠角" 英文翻译 :    wing-sweep actuation
• "后掠后掠角" 英文翻译 :    backswept
• "后缘后掠角" 英文翻译 :    trailing sweep
• "机翼后掠角" 英文翻译 :    wing sweep setting; wing-sweep angle
• "桨叶后掠角" 英文翻译 :    blade sweepback angle
• "零后掠角" 英文翻译 :    zero sweep
• "前翼后掠角" 英文翻译 :    forewing sweep
• "前缘后掠角" 英文翻译 :    leading edge sweep; leading sweep; leading-edge sweep angle
• "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
• "中等后掠角" 英文翻译 :    moderate sweep
• "变后掠角操纵" 英文翻译 :    sweep control
• "变后掠角机构" 英文翻译 :    sweep-angle change mechanism; variable-sweep mechanism
• "变后掠角手柄" 英文翻译 :    sweep lever
• "大后掠角布局" 英文翻译 :    highly swept configuration
• "桨叶尖后掠角" 英文翻译 :    blade tip sweepback
• "可变掠角水翼" 英文翻译 :    variable sweep hydrofoil
• "垂直尾翼后掠角" 英文翻译 :    fin sweep
• "改变后掠角的操作" 英文翻译 :    wing sweep operation
• "机翼变后掠角操纵" 英文翻译 :    wing sweep control

• Much more increase of maximum lift - to - drag ratio can be obtained with a forward - swept main wing with a small sweepback angle leading edge
  主机翼前掠角较小时，鸭翼改善和提高升阻比的效果比较明显。
• This paper has mainly made a research on the aerodynamic configuration design of " w " tailless aircraft and the design idea has been presented here . according to the configuration design requirement of certain uav , aerodynamic configuration design has been carried out and two configuration projects are given out at last : forward - swept wing tailless configuration and " w " tailless configuration . the longitudinal and lateral aerodynamic characteristics are obtained by using two aided soft : ug to build up geometrical models and mgaero to calculate flow field
  本文研究了“ w ”型无尾布局的气动外形设计，阐述了该布局的气动设计思想，根据型无人机的总体设计技术指标，进行了气动外形设计，提出了两种气动布局方案：前掠翼无尾气动布局和“ w ”型无尾气动布局，利用ug建模软件和mgaero气动分析计算软件计算了两种布局的纵、横向气动性能，分析了前掠翼前缘掠角和翼身融合对气动性能的影响，计算结果表明， “ w ”型气动布局的设计思想是正确的，所设计的“ w ”型无尾气动布局方案的气动性能优越，超过了总体设计技术指标。