Gas-Solid Spouted Rectangular Bed#
Features#
Solvers:
lethe-particles
andlethe-fluid-particles
Three-dimensional problem
Simulates a gas-solid spouted bed
Compares the simulation results to experimental results
Files Used in This Example#
The files mentioned below are located in the example’s folder (examples/unresolved-cfd-dem/gas-solid-spouted-rectangular-bed
).
Python functions script using Lagrangian post-processing:
functions_lagrangian.py
Python functions script using particles:
functions_particles.py
Parameter file for CFD-DEM simulation of the spouted bed:
gas-solid-spouted-rectangular-bed.prm
Parameter file for particle generation and packing:
packing-particles.prm
Python post-processing script using Lagrangian post-processing:
postprocessing_lagrangian.py
Python post-processing script using particles:
postprocessing_particles.py
Description of the Case#
This example simulates the spouting of spherical particles in air. The lethe-particles
solver is used to fill the bed with particles, then the lethe-fluid-particles
solver is used to simulate the spouting of the particles. Check-pointing is enabled in order to write the DEM checkpoint files to be used as the starting point of the CFD-DEM simulation. Using the parameters suggested by Geitani et al. [1], the simulation is run and the results are then compared to the experimental results from Yue et al. [2]
DEM Parameter File#
All parameter subsections are described in the parameter section of the documentation.
To set-up the rectangular spouted bed case, the bed is filled with particles to obtain a static bed height of 200 mm.
The different subsections of the parameter file packing-particles.prm
needed to run this simulation are introduced below.
Mesh#
The following figure shows the geometry of the mesh:

The dimensions shown in the figure are in millimeters, and the bed and the channel both have a depth of 40 mm. The flow is introduced through a channel that is connected to the bed. The geometry of the bed was created using GMSH. The mesh is created using the same dimensions as used by Geitani et al. [1] in order to compare the simulation results to the experimental results obtained by Yue et al. [2]. The mesh file is in the GMSH format and is located in the mesh
folder.
subsection mesh
set type = gmsh
set file name = ./mesh/spouted_structured.msh
set expand particle-wall contact search = false
end
Simulation Control#
In the simulation control
subsection, the time end
is set to 1.5 s with a time step
of 0.00001 s, which is long enough to allow the particles to come to rest. Additionally, users can specify the output folder for the simulation results in this subsection.
subsection simulation control
set time step = 0.00001
set time end = 1.5
set log frequency = 1000
set output frequency = 10000
set output path = ./output_dem/
end
Restart#
The lethe-fluid-particles
solver requires reading several DEM files to start the simulation. The check-pointing option is enabled in the restart
subsection.
subsection restart
set checkpoint = true
set frequency = 10000
set restart = false
set filename = dem
end
Model Parameters#
The following parameters are chosen for the model parameters
subsection. Dynamic load balancing is enabled to achieve better computational performance.
subsection model parameters
subsection contact detection
set contact detection method = dynamic
set dynamic contact search size coefficient = 0.9
set neighborhood threshold = 1.3
end
subsection load balancing
set load balance method = dynamic
set threshold = 0.5
set dynamic check frequency = 10000
end
set particle particle contact force method = hertz_mindlin_limit_overlap
set particle wall contact force method = nonlinear
set integration method = velocity_verlet
end
Lagrangian Physical Properties#
The gravitational acceleration as well as the physical properties of the particles and the walls are specified in the lagrangian physical properties
subsection. In order to obtain a static bed height of 200 mm, 175800 spherical particles with a diameter of 2.5 mm are inserted into the rectangular bed. All of the particle properties defined in this subsection are the same as those used by Geitani et al. [1]
subsection lagrangian physical properties
set g = 0.0, -9.81, 0.0
set number of particle types = 1
subsection particle type 0
set size distribution type = uniform
set diameter = 0.0025
set number = 175800
set density particles = 2500
set young modulus particles = 1e7
set poisson ratio particles = 0.25
set restitution coefficient particles = 0.9
set friction coefficient particles = 0.3
set rolling friction particles = 0
end
set young modulus wall = 1e7
set poisson ratio wall = 0.25
set restitution coefficient wall = 0.9
set friction coefficient wall = 0.3
set rolling friction wall = 0
end
Insertion Info#
The insertion info
subsection manages the insertion of particles. The volume of the insertion box is large enough to fit all the particles. The insertion info parameters are set in order to avoid particle collisions during the packing process.
subsection insertion info
set insertion method = volume
set inserted number of particles at each time step = 43950
set insertion frequency = 30000
set insertion box points coordinates = -0.139, 0.3, 0.001 : 0.139, 0.525, 0.039
set insertion distance threshold = 1.5
set insertion maximum offset = 0.3
set insertion prn seed = 19
end
Floating Walls#
A floating wall is used to prevent the particles from falling into the inlet channel. Its position is shown in the figure in the mesh subsection. The floating wall is defined at the top of the channel, which is at a y-coordinate of 0, and is set to remain active for the entire simulation time.
subsection floating walls
set number of floating walls = 1
subsection wall 0
subsection point on wall
set x = 0
set y = 0
set z = 0
end
subsection normal vector
set nx = 0
set ny = 1
set nz = 0
end
set start time = 0
set end time = 50
end
end
Running the DEM Simulation#
Assuming that the lethe-particles
executable is within your path, the simulation can be launched in parallel using the following command:
Note
Running the packing should take approximately 45 minutes on 10 cores.
After the particles have been packed inside the rectangular bed, it is now possible to simulate the spouting of the particles.
CFD-DEM Parameter File#
The CFD-DEM simulation is to be carried out using the packed bed simulated in the previous step.
Simulation Control#
The simulation is run for 10 s with a time step
of 0.0005 s. The time scheme chosen for the simulation is second order backward differentiation method (BDF2).
subsection simulation control
set method = bdf2
set output frequency = 50
set time end = 10
set time step = 0.0005
set subdivision = 1
set log precision = 10
set output path = ./output/
end
Physical Properties#
A density
of 1 and a kinematic viscosity
of 0.0000181 are defined in the physical properties
subsection to simulate the flow of air.
subsection physical properties
subsection fluid 0
set kinematic viscosity = 0.0000181
set density = 1
end
end
Initial Conditions#
A zero velocity field is used as the initial condition.
subsection initial conditions
subsection uvwp
set Function expression = 0; 0; 0; 0
end
end
Boundary Conditions#
The figure presented in the mesh subsection of this example shows the corresponding boundary IDs for each outer surface. A slip boundary condition is applied on all the walls of the bed and the channel (ID 0 and ID 3), except the inlet at the bottom of the channel (ID 1) and the outlet on the top of the bed (ID 2).
At the base of the channel, a time dependent Dirichlet boundary condition is imposed. To avoid an initial shock from the introduction of high velocity gas in the bed, the inlet is linearly velocity is increased from 0 m/s at t = 0 s until it reaches 20.8 m/s at t = 0.05 s.
subsection boundary conditions
set time dependent = true
set number = 4
subsection bc 0
set id = 0
set type = slip
end
subsection bc 1
set id = 1
set type = function
subsection u
set Function expression = 0
end
subsection v
set Function expression = if(t<0.05,416*t,20.8)
end
subsection w
set Function expression = 0
end
end
subsection bc 2
set id = 2
set type = outlet
end
subsection bc 3
set id = 3
set type = slip
end
end
The additional sections for the CFD-DEM simulations are the void fraction subsection and the CFD-DEM subsection. These subsections are described in detail in the CFD-DEM parameters .
Void Fraction#
Since the void fraction is calculated using the packed bed of the DEM simulation, the mode
is set to dem
. To read the dem files, read dem
is set to true
and the prefix of the dem files is specified. The quadrature centered method (QCM) is chosen to calculate the void fraction.
subsection void fraction
set mode = qcm
set read dem = true
set dem file name = dem
set l2 smoothing length = 0.0075
set particle refinement factor = 0
end
CFD-DEM#
In the cfd-dem
subsection, grad-div stabilization is enabled to improve local mass conservation, and the void fraction time derivative
is enabled to account for the time variation of the void fraction.
subsection cfd-dem
set grad div = true
set void fraction time derivative = true
set drag force = true
set buoyancy force = true
set shear force = true
set pressure force = true
set saffman lift force = false
set drag model = difelice
set coupling frequency = 100
set implicit stabilization = false
set grad-div length scale = 0.1
set vans model = modelA
end
Non-linear Solver#
The inexact_newton
solver is used to avoid the reconstruction of the system matrix at each Newton iteration. For more information about the non-linear solver, please refer to the Non-Linear Solver Section
subsection non-linear solver
subsection fluid dynamics
set solver = inexact_newton
set tolerance = 1e-6
set max iterations = 25
set verbosity = verbose
set matrix tolerance = 0.8
end
end
Linear Solver#
The linear solver is defined according to the parameters suggested by Geitani et al. [1] The absolute tolerance for the linear solver is set to a value 100 times smaller than the tolerance of the non-linear solver to ensure the non-linear solver converges.
subsection linear solver
subsection fluid dynamics
set method = gmres
set max iters = 200
set relative residual = 1e-4
set minimum residual = 1e-8
set preconditioner = ilu
set ilu preconditioner fill = 1
set ilu preconditioner absolute tolerance = 1e-10
set ilu preconditioner relative tolerance = 1
set verbosity = verbose
set max krylov vectors = 200
end
end
Running the CFD-DEM Simulation#
Assuming that the lethe-fluid-particles
executable is within your path, the simulation can be launched using the following command:
Note
Running the CFD-DEM simulation should take approximately 1.5 days on 10 cores.
Post-processing#
It is possible to run the post-processing code to post-process the particle velocities with the following line, with the simulation path as the argument:
The functions used in the post-processing script are defined in the functions-particles.py
file. This post-processing script reads the particle velocity data and plots the particle velocities as a function of the x-position in the bed for different y-heights.
It is also possible to run the post-processing code using the lagrangian post-processing output with the following line, with the simulation path as the argument:
The functions used in the post-processing script are defined in the functions-lagrangian.py
file. This post-processing script uses the average particle velocities at each mesh point to plot the particle velocities as a function of the x-position in the bed for different y-heights.
For more information about the Lagrangian post-processing, please refer to the Post-processing Section.
Important
You need to ensure that lethe_pyvista_tools
is working on your machine. Click here for details.
Results and Discussion#
Using the postprocessing_particles.py
post-processing script, the particle velocity magnitudes are plotted, in the following figure, as a function of the x-position in the bed, for different y-heights. The simulation is run with the Rong drag model to compare the results with the results obtained with the Di Felice drag model.
The experimental results from Yue et al. [2] are shown in the same figure for comparison. The standard deviation of the particle velocity magnitudes is shown as a shaded area around the average velocity magnitude. The two drag models lead to different results mainly at the center of the bed, where the spouting occurs, with the Rong drag model leading to higher particle velocity magnitudes than the Di Felice drag model. The particle velocity magnitudes are in good agreement with the experimental results, especially at the center of the bed, where the spouting occurs.
The following animation shows the spouting of the particles as the gas is introduced from the channel at the base of the bed. The void fraction profile is shown as well.