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首页> 外文期刊>Journal of propulsion and power >Large-Eddy Simulation of Coaxial LN2/GH2 Injection at Trans- and Supercritical Conditions
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Large-Eddy Simulation of Coaxial LN2/GH2 Injection at Trans- and Supercritical Conditions

机译:跨临界和超临界条件下同轴LN2 / GH2注入的大涡模拟

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摘要

Large-eddy simulations are carried out for the coaxial injection of liquid nitrogen and preheated hydrogen at supercritical pressures. The conditions are similar to that in typical liquid-propellant rocket combustors. By using nitrogen as a model gas, the mixing process is studied without the interference with chemical reactions. An analysis of the thermodynamic conditions that arise in the shear layer reveals that local phase separation may occur if the injection condition is transcritical. A novel volume-translation method on the basis of the cubic Peng-Robinson equation of state is introduced for the use in multispecies large-eddy simulations and is tested for both trans- and supercritical injection conditions. The new thermodynamic model corrects the deficiencies of the Peng-Robinson equation of state in the transcritical regime at minimal extra computational cost Two independently developed large-eddy simulation codes are used for the simulations and the results are compared. The outcome indicates that the flowfield is mainly controlled by the turbulence on the resolved scales, and an accurate model for the fluid's thermodynamic state is more important than the subgrid-scale turbulence model or the details of the code architecture. A comparison with available experimental data shows that important flow features are well predicted.
机译:对超临界压力下液态氮和预热氢的同轴注入进行了大涡模拟。条件类似于典型的液体推进剂火箭燃烧室中的条件。通过使用氮气作为模型气体,可以在不影响化学反应的情况下研究混合过程。对剪切层中出现的热力学条件的分析表明,如果注入条件是跨临界的,则可能发生局部相分离。介绍了一种基于三次态Peng-Robinson状态方程的新颖的体积平移方法,用于多物种大涡模拟中,并针对跨临界和超临界注入条件进行了测试。新的热力学模型以最小的额外计算成本纠正了跨临界状态下Peng-Robinson状态方程的不足,并使用了两个独立开发的大涡模拟代码进行了仿真,并对结果进行了比较。结果表明,流场主要受解析尺度上的湍流控制,并且流体的热力学状态的精确模型比亚网格尺度湍流模型或代码体系结构的细节更为重要。与可用实验数据的比较表明,重要的流动特征得到了很好的预测。

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  • 来源
    《Journal of propulsion and power》 |2016年第1期|46-56|共11页
  • 作者单位

    Universitaet der Bundeswehr Muenchen, 85577 Neubiberg, Germany;

    Universitaet der Bundeswehr Muenchen, 85577 Neubiberg, Germany;

    Institute of Aerodynamics and Fluid Mechanics, Technische Universitaet Muenchen, 85748 Garching bei Muenchen, Germany;

    Institute of Aerodynamics and Fluid Mechanics, Technische Universitaet Muenchen, 85748 Garching bei Muenchen, Germany,Faculty of Aerospace Engineering, Technische Universiteit Delft, Kluyverweg 1, 2629 HS Delft, The Netherlands;

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