入射正速度梯度燃料射流一次分裂的数值模拟

Tao Zhang , Weimin Wang , Zhenghuan Li , Haijun Zhang , Haiqiao Wei , Rundong Li , Chang Zhai
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引用次数: 0

摘要

为了研究燃料射流在具有正速度梯度的交叉气流中的破裂过程,将流体体积(VOF)方法和自适应网格技术相结合,模拟了气体和液体的两相流动。比较分析了匀速气流和正速度梯度气流下直接燃料射流的破裂和相应的流动特性。模拟结果表明,燃料柱的形态变化是由气液剪切和不对称气流漩涡等因素引起的。燃料射流经历了初级分裂,主要包括柱状分裂和表面分裂。柱状破裂主要是雷利-泰勒(R-T)不稳定性,而表面破裂主要是开尔文-赫姆霍兹(K-H)不稳定性。与均匀流相比,正速度梯度入流的膨胀角平均增加了 9.2%,表面波的波长平均增加了 34%。
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Numerical simulation of the primary breakup of fuel jet with incoming positive velocity gradient

To study the breakup process of fuel jets in air crossflow with a positive velocity gradient, the Volume of Fluid (VOF) method and adaptive grid technology are combined to simulate the two-phase flow of gas and liquid. A comparative analysis is conducted on the breakup and corresponding flow characteristics of direct fuel jets under uniform and positive velocity gradient airflow. The simulation results demonstrate that the morphological changes of the fuel column are caused by factors such as gas-liquid shear and asymmetric airflow vortices. The fuel jet undergoes primary breakup, which mainly contains columnar and surface breakup. The columnar breakup is dominated by Rayleigh-Taylor (R-T) instability, while the surface breakup is dominated by Kelvin-Helmholtz (K-H) instability. Compared with uniform flow, the expansion angle in the positive velocity gradient incoming flow increases by an average of 9.2%, and the wavelength of the surface wave increases by an average of 34%.

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