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# Combustion Chamber ANSYS Fluent CFD Simulation Training

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In this project a combustion chamber is simulated by ANSYS Fluent software.

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This product includes Geometry & Mesh file and a comprehensive Training Movie.

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## The assumption for Combustion Chamber CFD Simulation

There are several assumptions to solve the Combustion Chamber CFD Simulation:

1. The simulation is transient
2. The flow is Incompressible; hence, the solution is pressure-based.
3. We consider the effect of Earth’s gravity on problem-solving.

## Combustion Chamber CFD Simulation Procedure

### Step 1: Geometry

The geometry of the present model is 3-D and Design Modeler software designs it. Inside the combustion chamber, there are three main parts, including the air inlet pipe, the burner section, and the outlet pipe. Inside the chamber, there is a thin wall with several cavities of varying dimensions. The primary small cavities for cooling the chamber wall by layering flow and the next big ones are to keep the flame in the middle of the chamber.

### Step 2: Mesh

ANSYS Meshing software performs the meshing of the present model. The mesh type is unstructured. We use a triangular grid and the element number is 694928.

### Step 3: Set-Up

Here is a summary of the steps to define and solve the problem in the table:

 (Model) (Combustion Chamber) Turbulence k-epsilon k-epsilon RNG Standard wall function species transport Defined Species O2, CO, CO2, CH4, N2, H2O (vapor) Energy Equation on (boundary conditions) for combustion simulation Inlet mass flow inlet Combustion Simulation Inlet Air Mass Flow 0.02 kg.s-1 Temperature 300 K O2 mass fraction 0.23 N2 mass fraction 0.77 Inlet Fuel mass flow 0.0006 m.s-1 temperature 300 K CH4 mass fraction 1 O2 mass fraction 0 N2 mass fraction 0 Outlet Pressure outlet (Combustion Chamber) Outlet Air Relative Pressure 0 Pa O2 mass fraction 0.23 N2 mass fraction 0 Wall B.C Wall Heat Flux 0 (isolated) Diffuse zero Methods for combustion simulation Coupled Discretization momentum Second-order upwind pressure Second-order upwind energy Second-order upwind species transport Second-order upwind Turbulence kinetic energy equations First-order upwind Turbulence Waste Rate Equations First-order upwind initialization for combustion simulation Standard temp 300 K O2 0.23 Species 0

We apply the Standard Wall Function and K-epsilon RNG model for the turbulence equation since the flow inside the combustion chamber is relatively complex and the simulation is steady. We use the species Transport model and the species are O2, CO, CO2, CH4, N2, H2O (vapor) for this simulation (Combustion Chamber).

in this case, there are two steps methane air combustion, with six species involved in the reaction, namely: methane, Oxygen, nitrogen, water vapor, carbon dioxide, and carbon monoxide. The air mass flow inlet is 0.02 kg.s-1  and inlet air temperature is equal to 300 k. Mass fractions are .23 and .77 for oxygen and nitrogen, respectively. The fuel is methane and its inlet temperature is 300 k, also the flow rate is 0.0006 m.s-1. Ultimately, the walls are insulated and the solver method is coupled.

You can obtain Geometry & Mesh file, and a comprehensive Training Movie which presents how to solve the problem and extract all desired results.

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