Transport of inertial spherical particles in compressible turbulent boundary layers

被引:0
|
作者
Yu, Ming [1 ]
Zhao, Lihao [2 ]
Yuan, Xianxu [1 ]
Xu, Chunxiao [2 ]
机构
[1] China Aerodynam R&D Ctr, State Key Lab Aerodynam, Mianyang 621000, Peoples R China
[2] Tsinghua Univ, Inst Fluid Mech, Dept Engn Mech, Key Lab Appl Mech,Minist Educ, Beijing 100084, Peoples R China
基金
中国国家自然科学基金;
关键词
high-speed flow; compressible turbulence; particle/fluid flow; PREFERENTIAL CONCENTRATION; HEAVY-PARTICLES; QUIESCENT CORE; VELOCITY; SIMULATIONS; ENTRAINMENT; MECHANISMS; GENERATION; DEPOSITION; DISPERSION;
D O I
10.1017/jfm.2024.507
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In the present study, we perform direct numerical simulations of compressible turbulent boundary layers at free stream Mach numbers 2-6 laden with dilute phase of spherical particles to investigate the Mach number effects on particle transport and dynamics. Most of the phenomena observed and well-recognized for inertia particles in incompressible wall-bounded turbulent flows - such as near-wall preferential accumulation and clustering beneath low-speed streaks, flatter mean velocity profiles, and trend variation of the particle velocity fluctuations - are identified in the compressible turbulent boundary layer as well. However, we find that the compressibility effects are significant for large inertia particles. As the Mach number increases, the near-wall accumulation and the small-scale clustering are alleviated, which is probably caused by the variations of the fluid density and viscosity that are crucial to particle dynamics. This can be affected by the fact that the forces acting on the particles with viscous Stokes number greater than 500 are modulated by the comparatively high particle Mach numbers in the near-wall region. This is also the reason for the abatement of the streamwise particle velocity fluctuation intensities with the Mach numbers.
引用
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页数:38
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