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Using EES (or other) software, study the effect of variable specific heats on the thermal efficiency of the ideal Otto cycle using air as the working fluid. At the beginning of the compression process, air is at \(100 \mathrm{kPa}\) and \(300 \mathrm{K}\). Determine the percentage of error involved in using constant specific heat values at room temperature for the following combinations of compression ratios and maximum cycle temperatures: \(r=6,8,10,12\) and \(T_{\max }=1000,1500,2000,2500 \mathrm{K}\)

Short Answer

Expert verified
Solution: To determine the percentage of error, calculate the thermal efficiency of the Otto cycle considering both variable and constant specific heats. Then, use the formula for error to find the percentage of error between the two efficiencies: \( \text{error} = \frac{\eta_{var} - \eta_{const}}{\eta_{const}} \times 100\% \). Perform these calculations for each combination of compression ratios and maximum cycle temperatures.

Step by step solution

01

Calculate the thermal efficiency considering variable specific heats

To do this, use the formula for the thermal efficiency of the Otto cycle with variable specific heats: \(\eta_{var} = 1 - \frac{T_2 - T_1}{(T_3 - T_4) (\gamma} - 1)\), where \(T_1 = 300\,K\), \(T_2\), \(T_3\), and \(T_4\) are the temperatures at points 2, 3, and 4 of the Otto cycle, respectively, and \(\gamma\) is the ratio of specific heats, which varies with temperature. For each combination of compression ratio r and maximum cycle temperature \(T_{\max}\), we need to find the temperatures \(T_2\), \(T_3\), and \(T_4\) using the temperature ratios \(T_2/T_1 = (r)^{\gamma - 1}\), \(T_3/T_2 = (T_{\max}/T_2)\), and \(T_4/T_3 = (1/r)^{\gamma - 1}\). The value of \(\gamma\) for each combination must be obtained from the software.
02

Calculate the thermal efficiency considering constant specific heats

Use the formula for the thermal efficiency of the Otto cycle with constant specific heats: \(\eta_{const} = 1 - \frac{1}{r^{\gamma} - 1}\), where \(\gamma\) is the ratio of specific heats at room temperature (use the value provided by the software). For each combination of compression ratio and maximum cycle temperature, calculate the constant specific heat thermal efficiency using the given \(\gamma\).
03

Calculate the percentage of error

For each combination of compression ratio and maximum cycle temperature, find the percentage of error between the variable and constant specific heat efficiencies using the formula: \(\text{error} = \frac{\eta_{var} - \eta_{const}}{\eta_{const}} \times 100\%\) After performing the above steps, we can determine the percentage of error involved in using constant specific heat values at room temperature for each given combination of compression ratios and maximum cycle temperatures.

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Most popular questions from this chapter

An Otto cycle with a compression ratio of 10.5 begins its compression at \(90 \mathrm{kPa}\) and \(35^{\circ} \mathrm{C}\). The maximum cycle temperature is \(1000^{\circ} \mathrm{C}\). Utilizing air-standard assumptions, determine the thermal efficiency of this cycle using (a) constant specific heats at room temperature and (b) variable specific heats.

A turbojet is flying with a velocity of \(900 \mathrm{ft} / \mathrm{s}\) at an altitude of \(20,000 \mathrm{ft}\), where the ambient conditions are 7 psia and \(10^{\circ} \mathrm{F}\). The pressure ratio across the compressor is \(13,\) and the temperature at the turbine inlet is 2400 R. Assuming ideal operation for all components and constant specific heats for air at room temperature, determine ( \(a\) ) the pressure at the turbine exit, \((b)\) the velocity of the exhaust gases, and \((c)\) the propulsive efficiency.

Consider an aircraft powered by a turbojet engine that has a pressure ratio of \(9 .\) The aircraft is stationary on the ground, held in position by its brakes. The ambient air is at \(7^{\circ} \mathrm{C}\) and \(95 \mathrm{kPa}\) and enters the engine at a rate of \(20 \mathrm{kg} / \mathrm{s}\) The jet fuel has a heating value of \(42,700 \mathrm{kJ} / \mathrm{kg},\) and it is burned completely at a rate of \(0.5 \mathrm{kg} / \mathrm{s}\). Neglecting the effect of the diffuser and disregarding the slight increase in mass at the engine exit as well as the inefficiencies of engine components, determine the force that must be applied on the brakes to hold the plane stationary.

Helium is used as the working fluid in a Brayton cycle with regeneration. The pressure ratio of the cycle is 8 the compressor inlet temperature is \(300 \mathrm{K},\) and the turbine inlet temperature is \(1800 \mathrm{K}\). The effectiveness of the regenerator is 75 percent. Determine the thermal efficiency and the required mass flow rate of helium for a net power output of \(60 \mathrm{MW},\) assuming both the compressor and the turbine have an isentropic efficiency of \((a) 100\) percent and \((b) 80\) percent.

In an ideal Brayton cycle, air is compressed from \(100 \mathrm{kPa}\) and \(25^{\circ} \mathrm{C}\) to \(1 \mathrm{MPa}\), and then heated to \(927^{\circ} \mathrm{C}\) before entering the turbine. Under cold-air-standard conditions, the air temperature at the turbine exit is \((a) 349^{\circ} \mathrm{C}\) (b) \(426^{\circ} \mathrm{C}\) \((c) 622^{\circ} \mathrm{C}\) \((d) 733^{\circ} \mathrm{C}\) \((e) 825^{\circ} \mathrm{C}\)

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