3.4. CFD Guided Optimization of FBR Configuration
CFD simulation is divided into four stages, first step of which is Geometry. Geometry is the order of creating the shape to be actually analyzed or specifying conditions in flow analysis. In general, process drawings are often inserted into files or produced in the program itself. Since it is important to implement it under realistic conditions, the governing equations and numerical techniques that apply the flow conditions such as flow speed, pressure, and temperature, and the calculation conditions such as gap width, relaxation coefficient, and variable values are entered. In addition, boundary conditions must be specified to input the physical state and information of the fluid, which is the most important setting when performing simulation. First, in this study, velocity was used as the setting for the inlet condition, and pressure was used as the setting for the discharge water outlet. The reason for setting these boundary conditions is that they are applied according to the domain of the analysis target, which is common when rotation occurs in a structure due to a strong flow.
The second step is meshing, which specifies the part of the shape to be analyzed. There are significant differences in interpretation of the grid configuration of CFD depending on its shape and size. There are three types of grids, namely hexahedral, tetrahedral and pyramidal. In this study, the polyhedral shape was used. This shape was selected because it is commonly used to accurately calculate turbulence and fluid analysis. In the case of a hexahedral other than the target shape, the numerical analysis results can produce highly accurate results, but if the structure is complex or the flow changes significantly within a short period of time, many errors may occur in the connection and formation of the lattice, which can lead to large errors in actual crystals. Changes have the potential to cause large errors. In addition, in the case of tetrahedral, it is expected that the analysis time will be somewhat long as it is mainly used in structural analysis to perform accurate calculations on the boundary layer of the structure.
Typically, increased grid density correlates with improved accuracy; however, this negatively impact by increasing analysis times, necessitating the need for careful adjustments. In this study, for efficient calculations, the overall grid size was set to 5 mm, and a relatively dense grid was placed at the inlet and outlet where rapid changes in flow are expected, as well as the flow part of the crystal, to ensure efficient analysis time and detailed flow changes. The goal was to increase accuracy and reliability by enabling accurate predictions.
The third order is physics, which specifies all conditions and equations used in flow analysis. The conditions used in this study are shown in Table 1. The equation Lagrangian-mutiphase can analyze the interaction between the solid region of the crystal and the liquid region of the wastewater in the process and the flow rate and pressure of each phase. Therefore, an equation that analyzes two or more phases simultaneously was inserted.
In the case of equations, the continuity equation and momentum equation were calculated using the k-epsilon model for turbulence generated due to strong flow velocity. This model can be considered suitable for structural fluid analysis because it is an equation that provides a good compromise in terms of accuracy and stability in general-purpose simulation. The resulting equation is as follows (Eq. 2).
Equation for kinetic energy (K):
Where, ρ is the density of the fluid, t is time, u
i is the velocity component, xi is the coordinate, μ is the dynamic viscosity, μ
t is the turbulent viscosity, σ
K is the modeling constant of the turbulent viscosity, and P
K is the kinetic energy.
Equation for kinetic energy consumption rate (ε):
Where, Є represents turbulence energy (dissipation), σ
ε represents the modeling constant of turbulence energy, and C
1ε and C
2ε represent modeling constants. Afterwards, for particle analysis, analysis was performed using the Lagrangian method as shown in the equation below, and drag force (darg force, 𝐹
𝐷), lift force (𝐹
𝐿), and gravity force were considered as the forces acting on particles. The equation is as shown below (Eq. 4-6).
Where, 𝑑𝑝 and 𝐴𝑝 refer to the diameter and cross-sectional area of the particle. The particle diameter was 0.5 mm, the density was 2650 kg/m
3, and it was assumed to be silica sand. 𝐶𝐷 is the drag coefficient, and 𝑎
1, 𝑎
2, and 𝑎
3 are constants in the range of each constant 𝑅Є𝑝 number. 𝑅Є𝑝 refers to the Reynolds number of the particle.
Where, 𝑚
𝑝 and 𝑢
𝑝 mean the mass and speed of the particle, and Li and Ahmadi’s equation, which is a generalization of the equation called Saffman’s lift, was used. The constant K is 2.594, and 𝜌
𝑝 and 𝜈
𝑓 are the density of the particle and the fluid, respectively. It means kinematic viscosity coefficient.
Where, gi means force based on the law of universal gravitation.
The fourth step is to analyze the results of the actual flow inside the reactor. In general, the process of change due to flow can be confirmed in real time and predicted by analyzing the movement of a single grid.
The reactor configuration used in this study is depicted in Figure S1 along with all the dimensions. The FBR had a total height of 2,150 mm and a width of 50 mm. The silica particles were filled upto 500 mm height. The height of the lower part of the reactor was 95 mm and the fluid inlet part was 15 mm high and 29 mm in diameter. In order to verify the validity of the CFD program developed, comparative study between the experimental and model predicted results for increase in the seed bed height at different upflow velocities were conducted. The different upflow velocities used for this experiment were as follows: 10 m/h, 20 m/h, 30 m/h, 40 m/h, 50 m/h, and 60 m/h. In this numerical analysis, particle analysis was conducted after excluding energy loss due to flow rate and the possibility of crystal shape deterioration. Once the validity of the developed CFD model was established experiment was conducted to understand the effect of FBR configuration (bottom part angle and inlet diameter) on mixing inside the reactor. For this purpose, three different configurations were chosen, i.e., first existing reactor with inlet diameter of 29 mm, second a new FBR with lower angle of 12.6 degrees and inlet diameter of 29 mm, and third another FBR with a lower angle of 19.1 degrees and inlet diameter of 20 mm (Figure S2).
Further studies were conducted to find optimal design conditions using optimized CFD-DEM model. There are three design conditions that were optimized: (i) shape of the bottom of the reactor (according to the reactor bottom angle), (ii) diameter of the reactor inlet, and (iii) ratio of width to height of the reactor. For the first experiment, the bottom angle of the reactor was increased from 0° to 5°, 10° and 12.6° by keeping the inlet diameter fixed at 29 mm. Following this study, experiment was conducted to study the effect of inlet diameter by varying it from 29 mm to 25 mm, 23 mm and 20 mm. The ratio of width to height ratio was examined for three different ratios, viz, 1:43, 1:23 and 1:15. The reactor configuration for each of these experimental conditions are shown in Figure S2.
Table 1.
Conditions used for CFD flow analysis.
Table 1.
Conditions used for CFD flow analysis.
Condition (unit) |
Value |
Liquid density (kg/m3) |
997.561 |
Dynamic viscosity (Pa-s) |
8.8871 E-4 |
Cp (cal/g.k) |
0.998 |
Inlet velocity (m/s) |
4.7 E-4 |
Temperature (°C) |
25 |
Outlet pressure (Pa) |
0 |
Solid density (kg/m3) |
2,650 |
Solid diameter (mm) |
0.5 |
Number of grains |
20000 |
Particle count |
5000 |