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   线燃速 的翻译结果: 查询用时:0.274秒
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线燃速
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  linear burning rate
     An experimental device of linear burning rate of liquid monopropellant in high pressures was designed. The constant pressures were produced by coated propellant combustion in closed chamber. By use of measuring velocity technology of ion probe,the linear burning rate of OTTO Ⅱ was measured quantitatively at 45~83 MPa.
     该文设计了单元液体发射药高压线燃速试验装置 ,利用包覆火药柱在密闭爆发器中燃烧产生恒压环境 ,借助离子探针测速技术定量测试OTTO Ⅱ在 45~ 83MPa范围内的线燃速
短句来源
     The burning rate of energetic liquid is one of the key parameters to affect the combustion property of liquid propulsion system. A new device for measuring the linear burning rate of energetic liquid in high pressures was reported, i.e., the constant pressures were produced by coated propellant combustion. By use of the measuring velocity technology of ion probe, the linear burning rate of OTTO-Ⅱ was measured quantitatively at 55-122 MPa.
     报道了一种新型的含能液体高压燃速测量装置,即利用包覆火药燃烧产生恒压环境,借助离子探针测速技术定量测试OTTO Ⅱ在55~122MPa范围内的线燃速.
短句来源
  相似匹配句对
     ESTIMATE OF BURNING RATE OF PROPELLANT
     推进剂预估
短句来源
     ONLINE
     在线
短句来源
     A STUDY ON THE DESIGN OF A PERSONAL COMPUTER -BASED LINEAR CCD DATA ACQUISITION SYSTEM FOR COMBUSTION RATES OF CHARGES
     线阵CCD数据计算机采集系统的设计研究
短句来源
     The problems of burning rate correlation
     关于相关性问题
短句来源
     WIRE-SPEED PACKET INPUT PROCESSING
     线数据包输入处理技术
短句来源
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  linear burning rate
Under electron irradiation, the ignition temperature in the Ni-Al system decreases from 950 to 420 K, and the linear burning rate increases by a factor of 2-3 in an electric field with a frequency of 16 kHz.
      
In systems filled by inert additives, combustion of cellulose nitrate (CN) proceeds in a flameless low-temperature regime with a low linear burning rate.
      


Burning rate of liquid propellant is one of the key parameters to affect combustion property of liquid propellant.An experimental device of linear burning rate of liquid monopropellant in high pressures was designed.The constant pressures were produced by coated propellant combustion in closed chamber.By use of measuring velocity technology of ion probe,the linear burning rate of OTTO Ⅱ was measured quantitatively at 45~83 MPa.The results show that it is content with exponential burning rate formula.The burning...

Burning rate of liquid propellant is one of the key parameters to affect combustion property of liquid propellant.An experimental device of linear burning rate of liquid monopropellant in high pressures was designed.The constant pressures were produced by coated propellant combustion in closed chamber.By use of measuring velocity technology of ion probe,the linear burning rate of OTTO Ⅱ was measured quantitatively at 45~83 MPa.The results show that it is content with exponential burning rate formula.The burning rate coefficient and exponent are also calculated.The results are of great value to interior ballistic design of regenerative liquid propellant gun.

液体发射药燃速是影响液体发射药燃烧性能的关键参数之一。该文设计了单元液体发射药高压线燃速试验装置 ,利用包覆火药柱在密闭爆发器中燃烧产生恒压环境 ,借助离子探针测速技术定量测试OTTO Ⅱ在 45~ 83MPa范围内的线燃速。结果表明 ,它满足指数燃速公式 ,并算出了相应的燃速系数和燃速指数。研究结果对再生式液体发射药火炮内弹道设计有重要价值。

The burning rate of energetic liquid is one of the key parameters to affect the combustion property of liquid propulsion system. A new device for measuring the linear burning rate of energetic liquid in high pressures was reported, i.e., the constant pressures were produced by coated propellant combustion. By use of the measuring velocity technology of ion probe, the linear burning rate of OTTO-Ⅱ was measured quantitatively at 55-122 MPa. The results show that it is content with exponential burning rate law....

The burning rate of energetic liquid is one of the key parameters to affect the combustion property of liquid propulsion system. A new device for measuring the linear burning rate of energetic liquid in high pressures was reported, i.e., the constant pressures were produced by coated propellant combustion. By use of the measuring velocity technology of ion probe, the linear burning rate of OTTO-Ⅱ was measured quantitatively at 55-122 MPa. The results show that it is content with exponential burning rate law. Based on the experiment data, the burning rate coefficient and exponent were adapted. The research results can give basic data for the interior ballistic design of the liquid propulsion system.

报道了一种新型的含能液体高压燃速测量装置,即利用包覆火药燃烧产生恒压环境,借助离子探针测速技术定量测试OTTO Ⅱ在55~122MPa范围内的线燃速.结果表明,它满足指数燃速定律,并从试验数据拟合出燃速系数和燃速指数,其结果可为液体推进系统内弹道设计提供基础数据.

 
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