Numerical study on coupled flow characteristics of a gas-solid two-phase jet in a supersonic crossflow

被引:9
|
作者
Ding, Hongming [1 ]
Zhuo, Changfei [1 ]
Deng, Hanyu [1 ]
Hu, Wenjun [2 ]
Chen, Xiong [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Mech & Engn, Nanjing 210094, Peoples R China
[2] Yibin North Chuanan Chem Ind Co Ltd, Yibin 644219, Sichuan, Peoples R China
基金
中国国家自然科学基金;
关键词
Powder fuel; Multiphase flows; Particles flow; Supersonic flows; Transverse jets; SONIC INJECTION;
D O I
10.1016/j.ijmultiphaseflow.2023.104583
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this study, the Eulerian-Lagrangian scheme coupled with the gas-solid two-phase Reynolds-average Navier-Stokes (RANS) method was used to study the airflow and particles flow characteristics of particles of different diameters injected into a supersonic flow field by a sonic jet. The results show that introducing small particles has little effect on the flow field. When the particle diameter is 1e-6 m, most particles are mainly distributed in the shear layer, and some parts of the particles are sucked into the surface trailing counter-rotating vortex pairs (TCVP) and the wall boundary layers by the airflow. The introduction of large diameter particles hinders the jet's development, reduces the Mach disk's height, and makes the counter-rotating vortex pair (CVP) closer to the wall. This leads to a decrease in the streamwise velocity and an increase in the wall-normal velocity near the wall downstream of the jet. The streamwise velocity increases and the wall-normal velocity decreases at the far wall downstream of the jet. At the same time, it exacerbates the Kelvin-Helmholtz (K-H) instability in the shear layer on the windward side of the jet, forming a large-scale coherent structure between the shear layer and crossflow. The penetration depth and diffusion range of particles increase with particle diameter and density, and the velocity decreases with particle diameter increase by comparing the trajectories of particles with different di-ameters and densities.
引用
收藏
页数:18
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