发动机燃烧室的英文

• engine chamber
• motor chamber

• "发动机"英文翻译    engine; motor
• "燃烧室"英文翻译    combustion chamber; blast ch ...
• "发动机燃烧室直径" 英文翻译 :    motor chamber diameter
• "火箭发动机燃烧室" 英文翻译 :    chamber; rocket motor; rocket chamber; rocket-motor tube
• "主发动机燃烧室" 英文翻译 :    sustainer chamber
• "火箭发动机燃烧室壁冷却" 英文翻译 :    rocket wall cooling
• "火箭发动机燃烧室运动" 英文翻译 :    chamber movement
• "喷管收缩的发动机燃烧室" 英文翻译 :    mae west
• "绕丝火箭发动机燃烧室" 英文翻译 :    filament-wound rocket chamber
• "筒形火箭发动机燃烧室" 英文翻译 :    cylindrical rocket combustion chamber
• "涡轮喷气发动机燃烧室" 英文翻译 :    turbojet chamber
• "主发动机燃烧室壳体" 英文翻译 :    sustainer charge body tube
• "发动机燃烧" 英文翻译 :    cumbustion
• "冲压式空气喷气发动机燃烧室" 英文翻译 :    athodyd combustion chamber
• "发动机燃烧特性" 英文翻译 :    motor combustion characteristic
• "t形燃烧室发动机" 英文翻译 :    t head engine
• "单燃烧室发动机" 英文翻译 :    single-barreled motor
• "单燃烧室式发动机" 英文翻译 :    single-chamber engine
• "多燃烧室发动机" 英文翻译 :    multiple-chamber engine
• "共燃烧室发动机" 英文翻译 :    split single
• "三燃烧室发动机" 英文翻译 :    three-barrel engine; triple barrel motor; triple barreled motor; triple-barrel engine; triple-barrel motor
• "双燃烧室发动机" 英文翻译 :    twin combustion chamber motor; twin-combustion-chamber engine; two-barreled motor
• "四燃烧室发动机" 英文翻译 :    four-chamber engine
• "汽车发动机燃烧过程" 英文翻译 :    automotive engine combustion process
• "往复式发动机燃烧及排放" 英文翻译 :    reciprocating engine combustion and emission

• Study on primary combustion zone of aeroengine combustor
  航空发动机燃烧室主燃区特性的研究
• Transient dynamical analysis of aero - engine combustor outer casing
  航空发动机燃烧室外机匣瞬态动力分析
• Computer simulation of optimum time domain control for random combustor acoustic loading
  航空发动机燃烧室声载荷时域最佳控制的计算机仿真
• Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows
  本文通过数值模拟得到了超燃冲压发动机燃烧室化学反应流流场的流动结构。
• The ignition system provides high - voltage electric parks that ignite , or set fire to , the charges of air - fuel mixture in the engine combustion chambers
  点火装置产生高压电火花，从而使发动机燃烧室中的可燃混合气起燃。
• Mayer a e h j , stowe r a . experimental study into mixing in a solid fuel ducted rocket combustion chamber [ r ] . aiaa 2000 - 3346
  余勇,陈小前,等.三维实验固体火箭冲压发动机燃烧室湍流反应流数值模拟[ j ] .国防科技大学学报, 2002 , ( 5 )
• In the introduction the review of the research on a dual - mode scramjet combustor both abroad and domestic is presented and the main work of this paper is also presented briefly
  第一章为引言，简要回顾了国内外双模态冲压发动机燃烧室研究的现状，并在结尾介绍了本文的主要工作。
• The flow fields of two - dimension for fuel - air equivalence ratio = 0 . 35 are respectively calculated . comparisons made with experimental data obtained at similar ( but not identical ) flow conditions were encouraging
  得到了油气当量比= 0 . 35的氢燃料超燃冲压发动机燃烧室流场的精细结构。
• It puts forward an effective deep drawing technology about the alloy board with low - alloy and high - strength so that the properties of motor combustion chamber case satisfy with the needs of system
  从而提出了一套行之有效的低合金高强度合金板的拉深工艺，确保发动机燃烧室壳体的质量满足系统性能要求。
• The filament - wound case ( fwc ) plays a more and more important role in the solid rocket motor chamber structure ( srmcs ) with composite material widely used in spaceflight fields
  随着复合材料在各个领域的广泛应用，作为发动机燃烧室的纤维缠绕复合材料壳体在航天领域中越来越受到人们的重视。