An experimental study on turbulence modification in the near-wall boundary layer of a dilute gas-particle channel flow

2012 ◽  
Vol 53 (5) ◽  
pp. 1385-1403 ◽  
Author(s):  
Jing Li ◽  
Hanfeng Wang ◽  
Zhaohui Liu ◽  
Sheng Chen ◽  
Chuguang Zheng
Author(s):  
Sylvain Aguinaga ◽  
Olivier Simonin ◽  
Jacques Bore´e ◽  
Vincent Herbert

The deposition rate of droplets is strongly linked to their interaction with the boundary layer turbulence. In “industrial simulations”, droplets dispersion is usually modeled using Lagrangian stochastic simulations based on Reynold Average Navier Stokes (RANS) fluid calculations. Wall functions are also used to bound the number of mesh cells in the near wall region. But they also reduce the description of the boundary layer and lead to bad predictions of the droplets deposition rate. This study presents channel flow simulations using wall functions and run with the CFD code Fluent. In such configurations, the stochastic model of Fluent failed to represent the so-called “diffusion-impaction” regime of deposition. The “Concentration Wall Boundary Layer” model presented in this paper has been developed to predict deposition in simulations using industrial meshes with refinement such as y* > 20. This model calculates the deposition rate using only the intrinsic properties of the particles and the turbulent kinetic energy of the fluid expressed at the top of the boundary layer. The data provided by wall functions are then sufficient to calculate the deposition rate. This model is turned into a “Lagrangian stochastic wall boundary condition model” for the commercial CFD code Fluent. Various simulations have shown that this model improves remarkably the deposition predictions in channel flow. The dependence on the boundary cell size and the channel flow mean velocity has been tested. This model draws interesting perspectives to model deposition in complex configurations without requiring prohibiting mesh sizes.


2007 ◽  
Vol 33 (2) ◽  
pp. 173-175 ◽  
Author(s):  
S. V. Bulovich ◽  
V. É. Vikolaĭnen ◽  
S. V. Zverintsev ◽  
R. L. Petrov

1961 ◽  
Vol 83 (3) ◽  
pp. 371-377
Author(s):  
Ghassan Khabbaz ◽  
Yasutoshi Senoo

An experimental study of the influence of tip clearance on the stall limits of compressor blades was conducted on a rectilinear cascade. By using the mirror and image technique the end wall boundary layer near the clearance was dispensed with. The blade loading was maximum at a distance from the tip clearance, but the clearance was found to relieve the pressure gradient in general and to retard stalling.


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