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In an ideal Otto cycle, air is compressed from \(1.20 \mathrm{kg} / \mathrm{m}^{3}\) and 2.2 to \(0.26 \mathrm{L},\) and the net work output of the cycle is \(440 \mathrm{kJ} / \mathrm{kg} .\) The mean effective pressure (MEP) for this cycle is \((a) 612 \mathrm{kPa}\) \((b) 599 \mathrm{kPa}\) \((c) 528 \mathrm{kPa}\) \((d) 416 \mathrm{kPa}\) \((e) 367 \mathrm{kPa}\)

Short Answer

Expert verified
Answer: The mean effective pressure (MEP) of this Otto cycle is approximately 528 kPa.

Step by step solution

01

Calculate the initial and final volume of the air

We are given the initial density of the air \(\rho_i=1.20 \mathrm{kg/m^3}\) and we have to compress it to a final volume 0.26 L. The initial volume can be calculated using the ideal gas law: \(PV=mRT\). Here, \(P\) is pressure, \(V\) is volume, \(m\) is mass, \(R\) is the specific gas constant, and \(T\) is temperature. Since we are given the initial conditions, we can assume a mass of 1 kg for the air. Considering air to be an ideal gas, we can use the specific gas constant for air, \(R=287 \mathrm{J/kg K}\). We are given the initial pressure \(P_i=2.2\times10^5 \mathrm{Pa}\). We can now calculate the initial volume \(V_i\) as: \[V_i = \frac{m}{\rho_i} = \frac{1 \mathrm{kg}}{1.20 \mathrm{kg/m^3}} \approx 0.833 \mathrm{m^3}\] Since we are given the final volume \(V_f = 0.26 \times 10^{-3} \mathrm{m^3}\) (converting L to m³), we can now proceed to calculate the work done during compression and expansion.
02

Calculate the work done during compression and expansion

For an ideal Otto cycle, work done during the compression process \((W_C)\) and expansion process \((W_E)\) can be calculated using the following equations: \(W_C = mR(T_2-T_1)/(1 - k)\) and \(W_E = mR(T_4-T_3)/(1-k)\) where \(T_1, T_2, T_3, T_4\) are the temperatures at points 1, 2, 3, 4 (respectively), \(m\) is mass, \(R\) is the specific gas constant, and \(k\) is the specific heat ratio (for air, \(k=1.4\)). We have to find \(T_2 - T_1\) and \(T_4 - T_3\). We can use the relation: \(\frac{T_2}{T_1} = \frac{P_2}{P_1}(\frac{V_1}{V_2})\) and \(\frac{T_4}{T_3} = \frac{P_1}{P_2}(\frac{V_1}{V_2})\) Since we are not given temperatures, we can ignore the temperature terms and find the ratio of work done \((W_C)/(W_E)\): \[\frac{W_C}{W_E} = \frac{T_2-T_1}{T_4-T_3} \] To find \(W_C\) and \(W_E\), we are given the net work output of the cycle \((W_{net})\) as 440 kJ/kg. Since \(W_{net} = W_E - W_C\), we can find the ratio of work done: \[\frac{W_C}{W_E} = 1 - \frac{W_{net}}{W_E} \Longrightarrow W_E = \frac{W_{net}}{1-\frac{W_C}{W_E}}\]
03

Calculate the Mean Effective Pressure (MEP)

Mean Effective Pressure (MEP) is defined as the hypothetical constant pressure that, if maintained throughout the entire cycle, would result in the same amount of net work output. The formula for MEP is: \[MEP = \frac{W_{net}}{V_\text{displaced}}\] We know that \(W_{net}=440\,\text{kJ/kg}\). To find \(V_\text{displaced}\) (the difference in volume), we simply subtract the final volume from the initial volume: \[V_\text{displaced}=V_i-V_f \approx 0.833\,\text{m}^3 - 0.26 \times 10^{-3}\,\text{m}^3\] Now, we can find the MEP: \[MEP = \frac{440\times10^3\,\text{J/kg}}{0.833\,\text{m}^3 - 0.26 \times 10^{-3}\,\text{m}^3} \approx 528000\,\text{Pa} = 528\,\text{kPa}\] So the mean effective pressure (MEP) for this Otto cycle is approximately 528 kPa, which corresponds to the option (c).

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Engine Thermodynamics
Understanding the principles of engine thermodynamics is crucial for comprehending how energy is converted into work in engines like the ideal Otto cycle. The Otto cycle is a thermodynamic process typical for internal combustion engines and involves four distinct stages: intake, compression, power, and exhaust. During the intake, air (and usually fuel) is drawn into the engine. Compression then increases the pressure and temperature of the mixture, followed by ignition, which causes the power stroke as the gases expand. Finally, the exhaust stroke expels the burnt gases, and the process starts over.

The cycle is categorized as an ideal process, meaning it assumes no energy losses or inefficiencies. Real engines deviate from this ideal due to friction, heat loss, and other factors. However, examining the ideal cycle provides significant insight into engine operation, paving the way for real-world applications and improvements. Engine thermodynamics not only dictates the operation of these phases but also relies on principles such as the conservation of energy and the ideal gas law to predict the performance and efficiency of the engine.
Mean Effective Pressure
Mean Effective Pressure (MEP) is a critical term in the evaluation of an engine's performance. It represents the average pressure that acts on the pistons of an engine that would produce the same amount of work during one cycle as that produced under varying pressures. In simpler terms, it is a helpful way to summarize the net output of an engine in terms of a single, constant pressure value that equates to the same amount of work done over the entire cycle.

MEP is important as it provides an indication of an engine's capability to do work, regardless of its size. It allows for the comparison of engines on a common basis. For instance, when an Otto cycle operates, the MEP can be used to evaluate the effectiveness of the compression and power strokes by equating the net work done to a hypothetical constant pressure that could achieve the same result. The calculation of MEP, as seen in the exercise, considers the work done (energy output) and the volume displacement (space the piston travels), making it a comprehensive measure of engine efficiency.
Ideal Gas Law
The ideal gas law is a fundamental equation that is invaluable in fields such as engine thermodynamics. It relates the pressure (P), volume (V), temperature (T), and amount of substance (n) of an ideal gas through the equation:
\[PV = nRT\]
where R represents the gas constant, specific to the gas in question. In our engine context, it's common to calculate mass-based processes, using the mass (m) and specific gas constant (R), where R is tailored for units of mass rather than amount of substance, thus giving us the modified form:\[PV = mRT\]This law presupposes the gas being analyzed behaves ideally, which means its molecules do not attract or repel each other and take up a negligible space relative to the container. While no real gas is perfectly ideal, many behave ideally under common conditions, allowing this simplification to be useful for calculating changes in state during an engine cycle.

In the problem at hand, the ideal gas law was initially employed to calculate the volume of the air before compression, indicating its underlying importance in determining states from known quantities. It also permits the direct correlation between thermodynamic state variables, essential for analyzing changes during processes such as those within the Otto cycle.

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Most popular questions from this chapter

Do diesel or gasoline engines operate at higher compression ratios? Why?

Consider an ideal gas-turbine cycle with one stage of compression and two stages of expansion and regeneration. The pressure ratio across each turbine stage is the same. The highpressure turbine exhaust gas enters the regenerator and then enters the low-pressure turbine for expansion to the compressor inlet pressure. Determine the thermal efficiency of this cycle as a function of the compressor pressure ratio and the high-pressure turbine to compressor inlet temperature ratio. Compare your result with the efficiency of the standard regenerative cycle.

In an ideal Brayton cycle with regeneration, air is compressed from \(80 \mathrm{kPa}\) and \(10^{\circ} \mathrm{C}\) to \(400 \mathrm{kPa}\) and \(175^{\circ} \mathrm{C}\), is heated to \(450^{\circ} \mathrm{C}\) in the regenerator, and then further heated to \(1000^{\circ} \mathrm{C}\) before entering the turbine. Under cold-air-standard conditions, the effectiveness of the regenerator is (a) 33 percent \((b) 44\) percent \((c) 62\) percent \((d) 77\) percent \((e) 89\) percent

An air-standard cycle, called the dual cycle, with constant specific heats is executed in a closed piston-cylinder system and is composed of the following five processes: \(1-2 \quad\) Isentropic compression with a compression ratio \(r=V_{1} / V_{2}\) \(2-3 \quad\) Constant volume heat addition with a pressure ratio, \\[ r_{p}=P_{3} / P_{2} \\] \(3-4 \quad\) Constant pressure heat addition with a volume ratio \\[ r_{c}=V_{4} / V_{3} \\] \(4-5 \quad\) Isentropic expansion while work is done until \(V_{5}=V_{1}\) \(5-1 \quad\) Constant volume heat rejection to the initial state (a) Sketch the \(P\) -V and \(T\) -s diagrams for this cycle. (b) Obtain an expression for the cycle thermal efficiency as a function of \(k, r, r_{c},\) and \(r_{p}\) (c) Evaluate the limit of the efficiency as \(r_{p}\) approaches unity and compare your answer with the expression for the Diesel cycle efficiency. (d) Evaluate the limit of the efficiency as \(r_{c}\) approaches unity and compare your answer with the expression for the Otto cycle efficiency.

A stationary gas-turbine power plant operates on an ideal regenerative Brayton cycle \((\epsilon=100 \text { percent })\) with air as the working fluid. Air enters the compressor at \(95 \mathrm{kPa}\) and \(290 \mathrm{K}\) and the turbine at \(880 \mathrm{kPa}\) and \(1100 \mathrm{K}\). Heat is transferred to air from an external source at a rate of \(30,000 \mathrm{kJ} / \mathrm{s}\) Determine the power delivered by this plant (a) assuming constant specific heats for air at room temperature and ( \(b\) ) accounting for the variation of specific heats with temperature.

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