飞航导弹的英文

• cruising missile
  ◇飞航导弹潜艇 aerodynamic guided missile submarine

• "飞"英文翻译    fly; flit
• "航"英文翻译    boat; ship
• "导弹"英文翻译    guided missile
• "飞航导弹潜艇" 英文翻译 :    cruise missile submarine; cruise-missile submarine
• "掠海面飞航导弹" 英文翻译 :    sea-skimming missile
• "巡航导弹" 英文翻译 :    cruise mi ile; cruise missiles; cruise missle; cruise-type missile; ruise missiles
• "飞航式导弹" 英文翻译 :    aerodynamically unsupported missile; air-supported missile; aircraft type vehicle; guided bomber; missile plane; wing-borne missile; winged missile
• "地射巡航导弹" 英文翻译 :    ground-launched cruise missile
• "反舰巡航导弹" 英文翻译 :    ascm
• "空射巡航导弹" 英文翻译 :    missile
• "陆基巡航导弹" 英文翻译 :    ground-launched cruise missile
• "巡航导弹概论" 英文翻译 :    cruise missiles
• "巡航导弹蓝图" 英文翻译 :    f.o.f
• "巡航导弹潜艇" 英文翻译 :    cruise missile submarine
• "远程巡航导弹" 英文翻译 :    long-range cruise missile
• "增程巡航导弹" 英文翻译 :    ecm; ercm
• "战略巡航导弹" 英文翻译 :    strategic cruise missiles
• "中程巡航导弹" 英文翻译 :    medium-range cruise missile
• "洲际巡航导弹" 英文翻译 :    intercontinental cruise missile
• "飞航式导弹库" 英文翻译 :    cruise missile; doodlebug; fly bomb
• "007勇破巡航导弹" 英文翻译 :    never say never again
• "超音速巡航导弹" 英文翻译 :    navaho
• "地面发射巡航导弹" 英文翻译 :    ground-launched cruise missile
• "反舰艇巡航导弹" 英文翻译 :    anti-ship cruise missle
• "空中发射巡航导弹" 英文翻译 :    air-launched cruise missile

• Overload control for winged missile using intelligent resistance
  采用智能阻尼的飞航导弹过载控制
• Application database in simulation modeling for cruise missile
  数据库在飞航导弹仿真建模中的应用
• Great achievements have been made in developing antiship missiles over the past 40 years
  航天三院飞航导弹研制发展历程
• Winged missiles journal
  飞航导弹
• The empty weight to total weight ratio of subsonic maneuverable missile was given experimentally
  利用经验的预测方法对亚声速飞航导弹的空重比进行预测。
• The mission section , the constrain conditions , the weight composition of the maneuverable missile , and the model of used in turbofan engine maneuverable missile were presented
  简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。
• The cycle parameters of missile for turbofan engine were optimized for meeting the demand of maneuverable missile , and the developing trend of missile for turbofan engine was predicted
  根据飞航导弹的要求对涡扇发动机进行了循环参数优化选择并预测了未来涡扇发动机的发展趋势。
• The performance of next generation maneuverable missile was predicted by taking into account its important parameters such as lift to drag ratio , empty weight to total weight ratio and effective load
  在考虑导弹空重、有效载荷和气动特性的情况下，预测了未来先进飞航导弹的性能。
• By using the method of aircraft and turbofan engine integrated analysis , a model of maneuverable missile and turbofan engine integrated optimum design was developed and the computational examples and the analysis were presented
  摘要利用飞机涡扇发动机一体化设计的思路，建立了飞航导弹涡扇发动机一体化设计的优化设计模型并给出了算例和分析。
• By using the method of aircraft and turbofan engine integrated analysis , a model of maneuverable missile and turbofan engine integrated constrain analysis and mission analysis was developed and the computative examples and the analysis were given
  摘要利用飞机涡扇发动机一体化设计的思路，建立了飞航导弹涡扇发动机一体化设计的约束分析和任务分析模型并给出了算例和分析。

• 飞航导弹的法语：bombe-assaillante engin (à voilure, aérien, aérodynamique)