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A liquid octane (C8H18) enters a combustion chamber of a gas turbine stationary at 1 atm and 25 °C, and burns with 300% of excess air that enters the chamber in the same state.
Determine the heat of combustion if the products come out at 226.85 °C (kJ/kg)
Determine adiabatic flame temperature (°C)
Cp/R = A +BT +CT2 + DT-2 Where T is in K from 298 oK |
Name | Chemical formula | A | B*103 | C*106 | D*10+5 |
n-Octane | C8H18 | 4.108 | 70.567 | -22.208 | 0 |
Carbon dioxide | CO2 | 5.457 | 1.045 | 0 | -1.157 |
Nitrogen | N2 | 3.28 | 0.593 | 0 | 0.04 |
Oxygen | O2 | 3.639 | 0.506 | 0 | -0.227 |
Water | H2O | 3.47 | 1.45 | 0 | 0.121 |