Challenge

Week 10 - Simulating Combustion of Natural Gas.

Objective

To perform a combustion simulation on the combustor model and plot the variation of the mass fraction of the different species’ in the simulation using line probes at different locations of the combustor as shown in Fig. You need to plot for CO2, H2O, CH4, N2, O2, NOx emissions & Soot formation.

Geometry Preparation

This is the 3D geometry of a combustion chamber that we need to deal with, but for this combustion simulation to reduce the simulation cost we are using only a 2-D face of this geometry.

The 2-D geometry of the above 3-D geometry is as follow

Now, we need to Create Named Selection in the Meshing and named each face as Fuel_inlet, Air_inlet, Axis, Outlet, Walls

Now, we need to mesh the geometry for 1 mm Element size

and Turn on the capture proximity.

The Mesh thus obtained is

Now we open Fluent for further operations.

We use the

Type as Pressure based

Absolute Velocity Formulation

Steady- Time

2D Space -Axissymmetric

Enable Energy Equation

Viscous Model as K-Epsilon

The Species Model is edited as follows

Model- Species Transport

Reaction- Volumetric

Options- Inlet Diffusions, Diffusions Energy Source

Mixture Material - Methane-air

Turbulence - Eddy- Dissipation

Now, we need to turn on the Nox model and Soot Model

Now the boundary condition is to be set.

Air-Inlet

Velocty- 0.5 m/s

Temperature - 300k

Species - O2 - 0.23

Fuel- Inlet

velocity - 80m/s

Species

Ch4 -1

And Finally, we simulated for 1000 Iterations,

Results Obtained...

The Static Temperature Contour is

Residual Plot

Mass fraction of Pollutant NO

Mass Fraction of Soot

Methane Mass fraction

CO Mass fraction

CO2 Mass Fraction

H2O Mass fraction

N2 Mass Fraction

O2 Mass fraction

Mass fraction of pollutants NO

Now, for plotting the results at various locations, we have inserted lines on different locations, at 1mm 2mm 3mm 4mm 5mm, and 6mm.

The Graph of Results at 6 different locations of the chamber as follows

Ch4 Mass fraction

CO Mass Fraction

CO2 Mass fraction

H2O Mass fraction

N2 Mass fraction

O2 Mass Fraction

Mass fraction of Pollutant NO

Mass fraction of Soot

************************************** PART-2********************************************

A parametric study is performed to analyze the effect of water addition (5% to 30% of mole fraction) to the fuel inlet.

Mixture Material - Methane-air-2-step

Boundary Conditions

Fuel Inlet

Velocity - 80 m/s

Inlet Temp - 300K

RESULTS

DP0

Temperature Contour

Maximum temperature - 2312 K

Mass fraction of NO

Mass Fraction of Soot

Mass fraction chart of pollutant NO

Mass Fraction chart of soot

DP1

Temperature Contour

Maximum Temperature - 2290 K

Mass fraction of NO

Mass fraction of soot formation

Mass fraction Chart of NO

Mass Fraction Chart of Soot Formation

DP2

Temperature contour

Maximum Temperature - 2264K

Mass fraction of Soot

Mass fraction of Soot formation

Mass fraction chart of NO

Mass Fraction chart of soot formation

DP3

Temperature Contour

Maximum Temperature - 2230K

Mass fraction of NO

Mass fraction of Soot formation

Mass fraction chart of pollutant

Mass fraction chart of soot formation

DP4

Temperature Contour

Maximum Temperature - 2187K

Mass fraction of NO

Mass Fraction of Soot formation

Mass Fraction Chart of NO

Mass fraction Chart of SOOT formation

DP 5

Temperature Contour

Maximum Temperature - 2130 K

Mass fraction of NO

Mass fraction of Soot Formation

Mass fraction chart of NO

Mass fraction chart of soot formation

Conclusion

With the addition of water, the temperature of the gases at the outlet is decreased with the increase in the % of water. The maximum temperature observed is 2312k and the minimum temperature is 2179 K.

Latent heat absorption of water particles during the combustion will lower the temperature resulting in the reduction of pollutants NO. so pollutant NO emission decrease with an increase in the addition of water.

The temperature of CO2, H2O have similar contours, which means the species mass fraction depends on the effective combustion.

An Oscillatory decrease is observed in the formation of soot particles in the order of DP2>DP3>DP4>DP1, the lowest value observed is in DP0, where water percentage is 0

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