Chapter 15: Problem 72
Estimate the adiabatic flame temperature of an acetylene \(\left(\mathrm{C}_{2} \mathrm{H}_{2}\right)\) cutting torch, in \(^{\circ} \mathrm{C}\), which uses a stoichiometric amount of pure oxygen.
Chapter 15: Problem 72
Estimate the adiabatic flame temperature of an acetylene \(\left(\mathrm{C}_{2} \mathrm{H}_{2}\right)\) cutting torch, in \(^{\circ} \mathrm{C}\), which uses a stoichiometric amount of pure oxygen.
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Get started for freeA fuel is burned with 70 percent theoretical air This is equivalent to \((a) 30 \%\) excess air (b) \(70 \%\) excess air \((c) 30 \%\) deficiency of air \((d) 70 \%\) deficiency of air \((e)\) stoichiometric amount of air
An adiabatic constant-volume tank contains a mixture of \(1 \mathrm{kmol}\) of hydrogen \(\left(\mathrm{H}_{2}\right)\) gas and the stoichiometric amount of air at \(25^{\circ} \mathrm{C}\) and 1 atm. The contents of the tank are now ignited. Assuming complete combustion, determine the final temperature in the tank.
Propane \(\left(\mathrm{C}_{3} \mathrm{H}_{8}\right)\) is burned with 150 percent theoretical air. The air-fuel mass ratio for this combustion process is \((a) 5.3\) \((b) 10.5\) \((c) 15.7\) \((d) 23.4\) \((e) 39.3\)
Using EES (or other) software, write a general program to determine the heat transfer during the complete combustion of a hydrocarbon fuel \(\left(\mathrm{C}_{n} \mathrm{H}_{m}\right)\) at \(25^{\circ} \mathrm{C}\) in a steady-flow combustion chamber when the percent of excess air and the temperatures of air and the products are specified. As a sample case, determine the heat transfer per unit mass of fuel as liquid propane \(\left(\mathrm{C}_{3} \mathrm{H}_{8}\right)\) is burned steadily with 50 percent excess air at \(25^{\circ} \mathrm{C}\) and the combustion products leave the combustion chamber at \(1800\) \(\mathrm{K}\).
One \(\mathrm{kmol}\) of methane \(\left(\mathrm{CH}_{4}\right)\) is burned with an unknown amount of air during a combustion process. If the combustion is complete and there are \(1 \mathrm{kmol}\) of free \(\mathrm{O}_{2}\) in the products, the air-fuel mass ratio is \((a) 34.6\) (b) 25.7 \((c) 17.2\) \((d) 14.3\) \((e) 11.9\)
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