推进剂供给的英文

• propellant supply

• "推进剂"英文翻译    propellant; propellent; prop ...
• "供给"英文翻译    supply; provide; furnish; fe ...
• "低温推进剂供给" 英文翻译 :    cryogenic propellant management
• "推进剂供给管路" 英文翻译 :    propellant feed line
• "推进剂供给系统" 英文翻译 :    propellant feed system; propellant-feed system
• "液体推进剂供给系统" 英文翻译 :    liquid-propellant feed system
• "停止供给推进剂" 英文翻译 :    propellant cutoff
• "反应剂供给" 英文翻译 :    reactant supply
• "冷却剂供给" 英文翻译 :    coolant supply
• "氧化剂供给" 英文翻译 :    oxidizer feeding
• "推进剂挤压供给系统" 英文翻译 :    propellant-pressurized feed system
• "推进剂" 英文翻译 :    propellant; propellent; propulser; propulsive agent
• "推进剂；推进的" 英文翻译 :    propellant
• "冷却剂供给系统" 英文翻译 :    coolant supply system
• "氧化剂供给管路" 英文翻译 :    oxidizer feed line
• "安全推进剂" 英文翻译 :    safe propeller
• "板状推进剂" 英文翻译 :    sheet propeller
• "爆燃推进剂" 英文翻译 :    deflagrating propeller
• "倍基推进剂" 英文翻译 :    double-based propellant
• "超冷推进剂" 英文翻译 :    hydrogen propeller
• "触变推进剂" 英文翻译 :    thixotropic propellant
• "单基推进剂" 英文翻译 :    simple-base propeller; single-base propellants
• "单元推进剂" 英文翻译 :    katergol; mono propellant; monopropellant; self-contained propeller
• "单质推进剂" 英文翻译 :    monopropellant
• "导弹推进剂" 英文翻译 :    missile propeller

• The test equipment such as power supply system , ignition system , propellant supply system , arcjet thruster , thrust measuring device and vacuum system are introduced briefly
  简要介绍了实验所使用的设备，如电源系统、点火系统、推进剂供给系统、电弧加热式发动机、推力测量装置和真空系统。
• The two - dimensional axisymmetric subsonic - transonic - supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method . the profiles of density , velocity , temperature , pressure and mach number can be obtained by the computation . the computation grid and some computed results are given here . the test equipment such as power supply system , ignition system , propellant supply system , arcjet thruster , thrust measuring device and vacuum system are introduced briefly . some working phenomena of the arcjet are observed and discussed . three different kinds of instability appeared in the process of the experiments . except some important parameters are measured , it is found that the operating stability of argon is better than that of nitrogen
  对一实验电弧加热式发动机二维轴对称亚跨超音速流动进行了数值模拟，所采用的方法是矢通量分裂算法.通过计算可以得出密度、速度、温度、压力和马赫数的分布.给出了计算所使用的网格和一些计算结果.简要介绍了实验所使用的设备，如电源系统、点火系统、推进剂供给系统、电弧加热式发动机、推力测量装置和真空系统.对所观察到的一些工作现象进行了讨论.有三种不同的不稳定性出现于实验过程.除了所测量的一些重要参数，通过实验发现氩比氮工作更稳定