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Thermodynamic assessment of a nitro-organic plasma with an experimental design method

机译:实验设计方法评估有机硝基等离子体的热力学

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The modelling of the plasma ignition of gun propellants requires the thermodynamic properties of a plasma generated by a CHON organic compound. The electrothermal launcher produces pressures up to some hundreds of megapascals and temperatures up to some tens of thousands Kelvin. We have developed a code, ALJAN-EP, to calculate the thermodynamical equilibrium for a CHON plasma by extension of the conventional method of minimisation of the enthalpy. We have presented results of calculation of the enthalpy and the isobaric thermal capacity for a nitrocellulose up to 500 MPa and 50000 K. Furthermore, we have used ALJAN-EP to determine polynomial expressions for a model of the second order in pressure and in temperature by experimental design. These expressions allow thermodynamic state functions and the composition of the gaseous phase to be calculated quickly and accurately. We present results obtained for nitrocellulose in a small temperature and pressure range from 100 to 500 MPa and 5000 to 10000 K. These results show that to cover a wider area, considering reactions in gaseous phase, it is necessary to consider a mosaic of adjacent elementary areas in parameter space or a more complex expression.
机译:枪支推进剂等离子体点火的建模需要CHON有机化合物生成的等离子体的热力学特性。电热发射器产生的压力高达数百兆帕,温度高达数万开氏温度。我们已经开发了一个代码ALJAN-EP,可以通过扩展使焓最小的常规方法来计算CHON等离子体的热力学平衡。我们已经给出了高达500 MPa和50000 K的硝酸纤维素的焓和等压热容量的计算结果。此外,我们使用ALJAN-EP确定了压力和温度下的二阶模型的多项式表达式,实验设计。这些表达式允许快速而准确地计算出热力学状态函数和气相组成。我们介绍了硝酸纤维素在100至500 MPa和5000至10000 K的小温度和压力范围内获得的结果。这些结果表明,考虑到气相反应,要覆盖更宽的区域,有必要考虑相邻元素的镶嵌参数空间中的区域或更复杂的表达式。

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