In: Chemistry
Given data:
Methane flowrate = 1000 kmol/hr
Air inlet composition, N2 = 80% and O2 = 20%
Total conversion percentage = 95%
Total del.p = 10 kpa
Pressure = 1 atm.
Assumption for the simulation:
Inlet temperature = 25 ° C
Let us write down the balanced reaction,
CH4 + 2 (O2 + 4N2) = CO2 + 2H2O (Since, Air contains 20 % O2 and 80% N2, so 20/20 O2 and 80/20 N2)
CH4 + 10 Air = CO2 + 2H2O
therefore, 1 kmol of methane requires 10 kmol of air for the reaction to complete with 100 % conversion, so here only 95% conversion, thus the required mole flow of air = 1000 * 9.5 = 9500 kmol of air.
The results I got from the simulation is,
Results:
1. Properties of exhaust gases such as average specific heat, enthalpy, entropy, thermal conductivity, viscosity etc.
Mass specific heat = 1.682 kJ/kg °C
Mass enthalpy =-258.8 kJ/kg
mass entropy = 8.484 kJ/kg °C
thermal conductivity = 0.07906 W/m K
viscosity = 0.07944 cP
2- Composition of exhaust gases from the burner in mole% and mass% =
mole%
CH4 =0.48 %
O2 = 0%
H2O = 18.1%
CO2 = 9.05%
N2 = 72.38%
Mass %:
CH4 =0.28 %
O2 = 0%
H2O = 11.81%
CO2 = 14.43%
N2 = 73.48%
3- The flow rate of each component in the exhaust gas in Kg/h
Methane 802.145 kg/h
Nitrogen 212898.80 kg/h
Oxygen 0 kg/h
CO2 41809.21 kg/h
H2O 34228.69 kg/h
4- Temperature of exhaust gases
Temperature = 1943 ° C
5- Pressure of exhaust gases
Pressure = 0.9133 bar
6- Volumetric flow rate of gases
Volume flow of gase = 2118495.88 m3/hr