Hydrogen Combustion in a Furnace CFD Simulation, ANSYS Fluent

Description

Hydrogen Combustion in a Furnace with Integration of the Sutherland viscosity and kinetic theory of thermal conductivity

Description

In recent decades, the numerical simulation of the combustion process has become one of the most important methods in the design of various systems. These modeling, if they have high accuracy, can provide many details of the complexity of the physicochemical process. Thus, when considering real issues such as pollution, ignition and extinction, the simulation method must be done accurately, so that reliable results can be obtained. The bulk viscosity is one such process to increase accuracy in simulation, that is produced by viscous forces that arise when a volume of fluid is compressed or dilated. Viscosity plays a major role in combustion in terms of fluid properties. In other words, the viscosity is one of the most important components of the coupling of turbulence and combustion. On the other hand, the kinetic theory of gases provides us with a relatively complementary framework for calculating the thermal conductivity in combustion problems. In this project, the combination of Sutherland viscosity and kinetic theory for thermal conductivity is presented for the accurate simulation of the combustion process. Therefore, the chemical reaction in the one-stage combustion of air/hydrogen has clearly shown the physical and chemical phenomena.

The design of a furnace with separate inlets of fuel and air is shown in the fig. 1. Inlet mass flow rate is set for hydrogen and air inlet, and for the outlet, the boundary condition of the outlet pressure and depletion to the atmosphere is considered. The mass flow rate is set to 0.01 Kg/s for air, and 0.0003 Kg/s for hydrogen, in which case the equivalence ratio is equal to 1. The boundary conditions of the side walls are all of the type of heat loss with the outside environment through convection and radiation (With the heat transfer coefficient of 16 W/m2/K, the ambient temperature is 300 K and the sky temperature is 271.2 K). Also, a thickness of 5 cm of shell condition type and steel metal is considered for the side walls.

The structured grid is used to create a mesh (in ANSYS Meshing software) in the computing domain (Fig. 2). In addition to the representation of the computing mesh, the dimensions are also shown in Fig. 2. Also, besides the dimensions shown, the distance from the center of the fuel inlet to the bottom of the furnace is 0.25 m, and this inlet is also located in the center of the air inlet. Nevertheless, the structured grid with a high quality will follow out the simulation of the combustion process as accurately as possible.

Results

The simulations are conducted in such a way that a non-premixed air-hydrogen mixture, with an equivalence ratio of 1, enters the furnace, and after the chemical reactions are completed, the combustion products are depletion to the atmosphere at the outlet. In this way, the properties of the non-premixed mixture, which is modeled by species transport, are given in the table 1.

The standard k-e turbulence model is used to simulate the combustion process. The volumetric reaction has been performed by activating the diffusion of the energy source and the turbulence-chemistry interaction of the eddy dissipation type. The SIMPLE algorithm is used for pressure and velocity coupling in the solution method section. Least Squares Cell Based is also considered for discretization of gradients, Second Order for pressure and Second Order Upwind for other variables. The Under relaxation factors are arranged such that convergence has taken place to the desired extent.

Velocity and temperature curves on the center line of fuel inlet are illustrated in Fig. 3. The maximum velocity was 1063 m/s at the fuel inlet, and the maximum temperature obtained 1860 K.

Mass fraction of H₂ and H₂O curves on the center line of fuel inlet are shown in Fig. 3. The mass fraction of H₂ at inlet 1, and on the facing surface is zero. On the other hand, the mass fraction of H₂O at the entrance of the furnace is zero, and after passing 0.3 m, it has reached a constant value of 0.23.

The maximum reaction rate also occurred at a distance of 2 cm from the entrance, which is 0.23 kmol/m³/s. After a distance of 0.4 meters, the reaction rate has reached zero, which indicates the completion of the flame.

The volume temperature contour in the furnace is also shown in the Fig. 6. The maximum temperature inside the furnace has reached 2102.56 Kelvin. On the other hand, a higher average temperature is observed in the lower part of the furnace.

The isotherm and thermal behavior in the inner of the furnace are also shown in Fig. 7. The planes on which the contours are displayed are placed at a distance of 0.125 meters from each other. It can be seen that the maximum temperature of 2080 K was obtained in the simulation.

Velocity contour is displayed from zero to maximum (Fig. 8-A), and from zero to 100 m/s (Fig. 8-B). In Fig. 8-B below, due to the display of flow behavior at lower speeds, the maximum value of this parameter is limited.

In the Fig. 9, the mass fraction of the combustion components is shown on the middle plate of the furnace (Symmetry surface).

Eddy viscosity represents the turbulent kinetic energy, is shown in Fig. 10. The kinetic energy of the flow (due to the eddy viscosity) is converted into internal energy, which this phenomenon is also known as energy cascade.

Conclusion

In this project, non-premixed hydrogen/air combustion in a furnace with laboratory scale or even semi-industrial dimensions is modeled by the eddy dissipation method. The eddy dissipation method is based on the fact that the process of species transfer in chemical reactions is done quickly. Therefore, the reaction rate related to the timescales of turbulent is considered. If the chemical reaction of fuel and oxidant molecules takes place in a large space with atmospheric pressure(such as furnaces), this method will be accurate enough to simulate their behavior and release energy source.

In this project, the combustion of stoichiometric non-premixed mixture of air/hydrogen is simulated in a furnace with dimensions of 0.6×0.3×0.5 m. The mass flow rate and temperature of the air at the inlet are considered to be 0.01 Kg/s and 300 K, respectively. The fuel temperature at the inlet is considered to be the same as the air temperature. The results with high accuracy indicate the precise settings of the software and the convergence of the solution. With using the eddy dissipation method, the relationship between the energy cascade and the high temperature domain of the furnace is clearly shown in the results. However, the reaction rate, mass fraction of the reactants component, temperature and velocity show the high accuracy of the simulation.