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航空煤油JP-10热物性的分子动力学模拟研究
Molecular Dynamics Simulation of Thermal Properties of Aviation Kerosene JP-10
【摘要】 燃料性能是决定远距离、大推力的推进系统效果的关键。由于实际工程应用中存在极端温度和压力,很难通过实验获得国产航空煤油JP-10的热物性参数,限制了其在航空航天领域中的应用。基于此,本文采用分子动力学模拟,探究300 K,1.48MPa条件下,不同时间步长(0.1 fs和1 fs)与不同力场(GAFF2和OPLS)对JP-10动力黏度和热导率的影响。结果表明,综合计算成本和误差各方面考虑,在1 fs下使用OPLS力场描述JP-10物性变化更为合适,为含能颗粒凝胶燃料的雾化燃烧研究提供了技术支撑。
【Abstract】 Fuel performance is the key factor in determining the effectiveness of propulsion systems for long-distance and high-thrust applications. Due to extreme temperatures and pressures in practical engineering applications, it is difficult to obtain the thermal and physical property parameters of domestic aviation kerosene JP-10 through experiments, which limits its use in aerospace fields. To address this, this study uses molecular dynamics simulations to investigate the effects of different time steps(0.1 fs and 1 fs) and different force fields(GAFF2 and OPLS) on the dynamic viscosity and thermal conductivity of JP-10 under conditions of 300 K and 1.48 MPa. The results show that,considering both the computational cost and error, using the OPLS force field with a time step of 1 fs is more suitable for describing the property changes of JP-10. This provides technical support for the study of atomized combustion of energetic particle gel fuels.
【Key words】 aviation kerosene JP-10; molecular dynamics simulation; OPLS force field; dynamic viscosity; thermal conductivity;
- 【文献出处】 工程热物理学报 ,Journal of Engineering Thermophysics , 编辑部邮箱 ,2026年02期
- 【分类号】V312
- 【下载频次】33