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Assessment and Validation of Internal Aerodynamics and Mixture Preparation in Spark-Ignition Engine Using LES Approach

机译:使用LES方法评估和验证火花点击引擎中内部空气动力学和混合物制备

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摘要

A workflow for the assessment and validation of internal aerodynamics and mixture preparation in a representative high-tumble optical engine using Large Eddy Simulation with the commercial code CONVERGETM is proposed. First, the prediction of the aerodynamic movement in the engine is compared to Particle Image Velocimetry (PIV) measurements. The global velocity fields and position of the center of the tumble for the average experimental and simulation cycles are compared, showing a very good match of the global behavior. The cycle to cycle aerodynamic variability is investigated thanks to velocity profiles, showing that the simulated cycles feature comparable velocity fluctuations to the experiments. In a second part, to account for Direct Injection (DI), a Lagrangian spray modeling approach is used to take into account the injection process. Experimental spray penetration data are used for the calibration of the spray models, leading to a faithful representation of the spray. Mixture preparation in the engine is then assessed, comparing the fuel air equivalence ratio of the LES in the central plane to LIF diagnostics. This qualitative comparison shows a good prediction of the evolution of the position of the fuel-rich areas and overall mixing during the compression stroke. The cycle to cycle variability of the mixing process is found comparable to the experiments, though underestimated. An evaluation of this methodology is given and the next steps towards combustion computations are discussed.
机译:提出了用于评估和验证内部空气动力学和混合物制备的工作流程,并提出了使用大型涡流模拟与商业代码convengetM的大型涡流仿真的工作流程。首先,将发动机中空气动力运动的预测与粒子图像速度法(PIV)测量进行了比较。比较了平均实验和仿真周期的全局速度场和滚筒中心的位置,显示了全球行为的很好匹配。由于速度曲线,研究了循环到空气动力学变异性的循环,表明模拟周期具有与实验相当的速度波动。在第二部分中,要考虑直接注射(DI),使用拉格朗日喷涂模型方法来考虑注射过程。实验喷雾渗透数据用于校准喷雾模型,从而导致喷雾的忠实表示。然后评估发动机中的混合物制备,比较中央平面中LES与LIF诊断的燃油空气等效比。这种定性比较表明了对燃料富集区域的位置的演变和压缩冲程过程中的整体混合的良好预测。发现混合过程的循环变异性与实验相当,尽管被低估了。对此方法进行了评估,并讨论了燃烧计算的下一步。

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