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Numerical aspects for physically accurate direct numerical simulations of turbulent jets

机译:湍流射流物理精确直接数值模拟的数值方面

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Numerical simulations of turbulent isothermal round jets are performed at Reynolds number (based on jet diameter and jet orifice velocity) of 5000 and Mach number of 0.6 to assess influences of initial perturbation, numerical discretization, and boundary treatments on turbulence statistics. The paper documents preliminary results from an investigation eventually aimed at examining multicomponent species injection and mixing at high-pressure conditions relevant to combustion in diesel, gas-turbine and liquid-rocket engines. Lack of reliable experimental or computational results at high pressures of interest make code validation at those conditions infeasible. Therefore, single-species simulations at perfect-gas conditions are first performed to assess turbulence statistics sensitivity to numerical setup. Two cases with different inflow velocity perturbation amplitude are considered to examine influences on jet flow transition and self-similarity.
机译:湍流等温圆形射流的数值模拟是在雷诺数为5000(基于射流直径和射流速度)和马赫数为0.6的情况下进行的,以评估初始扰动,数值离散化和边界处理对湍流统计的影响。该文件记录了一项研究的初步结果,该研究最终旨在检查在与柴油机,燃气轮机和液体火箭发动机的燃烧有关的高压条件下的多组分物质注入和混合。在感兴趣的高压下缺乏可靠的实验或计算结果,使得在这些条件下进行代码验证不可行。因此,首先在理想气体条件下进行单物种模拟,以评估湍流统计数据对数值设置的敏感性。考虑两种不同的入流速度扰动幅度的情况,以研究对射流过渡和自相似性的影响。

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