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Large eddy simulation of fuel injection under trans/supercritical conditions

机译:燃料喷射的大涡仿真在反式/超临界条件下

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The n-heptane jet with subcritical and supercritical inlet temperatures injected into a supercritical environment filled with multi-component gas, has been numerically investigated using large eddy simulation. Mainly attentions are paid on the effects of density-gradient, thermodynamic and transport properties on the flow evolution. We find that large density-gradients are easier formed in transcritical injection and the larger specific heat has the effects of increasing the density gradients. While the diffusion coefficient decrease in the larger density gradient regions, suggesting that large density gradient has the effects of suppressing the flow diffusion mixing. In addition, when the fluid transits across the pseudo boiling temperature, the specific heat obtained a maximum value, while this value is suppressed by the dissolution effects, indicating that multi-component injection is different from the single species injection and a special investigation is needed.
机译:使用大涡模拟已经在数值上研究了具有亚临界和超临界入口温度的N-庚烷射流,其填充有多组分气体的超临界环境。主要关注密度梯度,热力学和运输性能对流动演化的影响。我们发现跨临界注射中的大密度梯度更容易,并且较大的比热量具有增加密度梯度的效果。虽然较大密度梯度区域的扩散系数降低,但是提示大密度梯度具有抑制流动扩散混合的效果。另外,当流体跨越伪沸腾温度时,比热量获得最大值,而该值被溶出效应抑制,表明多分量注射与单一物种注射不同,需要进行特殊调查。

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