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A fuel at 25 \(^{\circ} \mathrm{C}\) is burned in a well-insulated steady-flow combustion chamber with air that is also at \(25^{\circ} \mathrm{C}\). Under what conditions will the adiabatic flame temperature of the combustion process be a maximum?

Short Answer

Expert verified
Answer: To achieve the maximum adiabatic flame temperature in a combustion process, the following conditions must be satisfied: 1. Both fuel and air should enter the combustion chamber at 25 °C. 2. The combustion process should be complete. 3. The ratio of fuel and air entering the combustion chamber should be stoichiometric, ensuring complete combustion without any excess air or fuel that could remove heat from the combustion zone.

Step by step solution

01

Identify the factors influencing adiabatic flame temperature

The adiabatic flame temperature depends on multiple factors such as the composition of the fuel and air, their initial temperatures, and the ratio of fuel and air entering the combustion chamber.
02

Understand fuel and air ratio

The ratio of fuel and air entering the combustion chamber is a key factor that affects the flame temperature. The stoichiometric ratio is the ideal ratio where fuel combines completely with oxygen in air, producing the maximum possible heat release. This ratio is critical for our analysis.
03

Identifying conditions

To maximize the adiabatic flame temperature: 1. Both fuel and air should be at 25 \(^{\circ} \mathrm{C}\). (As given in the problem statement) 2. The combustion should be complete so that the maximum possible chemical energy is released as heat. 3. The fuel and air mixture should be stoichiometric so that there is no leftover oxygen or fuel that could carry away heat with their exit from the combustion chamber. This means that there should be just enough air to completely burn all the fuel without any excess.
04

Conclusion

The maximum adiabatic flame temperature in the combustion process will be achieved under the following conditions: 1. Both fuel and air should enter the combustion chamber at 25 \(^{\circ} \mathrm{C}\). 2. The combustion process should be complete. 3. The ratio of fuel and air entering the combustion chamber should be stoichiometric, ensuring complete combustion without any excess air or fuel that could remove heat from the combustion zone.

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Most popular questions from this chapter

Acetylene gas \(\left(\mathrm{C}_{2} \mathrm{H}_{2}\right)\) at \(25^{\circ} \mathrm{C}\) is burned during a steady-flow combustion process with 30 percent excess air at \(27^{\circ} \mathrm{C} .\) It is observed that \(75,000 \mathrm{kJ}\) of heat is being lost from the combustion chamber to the surroundings per kmol of acetylene. Assuming combustion is complete, determine the exit temperature of the product gases.

A gaseous fuel with a volumetric analysis of 45 percent \(\mathrm{CH}_{4}, 35\) percent \(\mathrm{H}_{2},\) and 20 percent \(\mathrm{N}_{2}\) is burned to completion with 130 percent theoretical air. Determine \((a)\) the air-fuel ratio and ( \(b\) ) the fraction of water vapor that would condense if the product gases were cooled to \(25^{\circ} \mathrm{C}\) at 1 atm.

A gaseous fuel mixture that is 40 percent propane \(\left(\mathrm{C}_{3} \mathrm{H}_{8}\right)\) and 60 percent methane \(\left(\mathrm{CH}_{4}\right)\) by volume is mixed with the theoretical amount of dry air and burned in a steady-flow, constant pressure process at 100 kPa. Both the fuel and air enter the combustion chamber at \(298 \mathrm{K}\) and undergo a complete combustion process. The products leave the combustion chamber at 423 K. Determine (a) the balanced combustion equation, (b) the amount of water vapor condensed from the products, and \((c)\) the required air flow rate, in \(\mathrm{kg} / \mathrm{h},\) when the combustion process produces a heat transfer output of \(140,000 \mathrm{kJ} / \mathrm{h}\).

What does the dew-point temperature of the product gases represent? How is it determined?

Develop an expression for the higher heating value of a gaseous alkane \(C_{n} H_{2 n+2}\) in terms of \(n\).

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