物理
马赫数
机械
超音速
斯托克斯数
涡流
喷射(流体)
大涡模拟
湍流
经典力学
雷诺数
作者
Kangchun Zhao,Zhixun Xia,Likun Ma,Yifan Duan,Jiarui Zhang,Yunchao Feng,Binbin Cheng,Pengnian Yang
出处
期刊:Physics of Fluids
[American Institute of Physics]
日期:2023-01-20
卷期号:35 (2)
被引量:13
摘要
Large eddy simulation is used to study the gas-particle two-phase transverse jet in supersonic flow. In this paper, the Eulerian method is used to simulate the fluid, and the Lagrangian method is used to simulate the particles. The numerical study is carried out for different particle mass fractions and Stokes numbers with the jet-crossflow momentum flux ratio and the Mach number of crossflow being kept constant. It is found that the larger particles (St = 5) are mainly located above the counter-rotating vortex pair, and the smaller particles (St = 0.9) are mainly located in the counter-rotating vortex pair. Due to the Kelvin–Helmholtz instability, several characteristic phenomena have been observed, including particle trailing and the wave structure constructed of the particle cloud, and the particles also make the Mach disk lower.
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