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At the beginning of the compression process of an airstandard Otto cycle, \(p_{1}=1\) bar, \(T_{1}=290 \mathrm{~K}, V_{1}=400 \mathrm{~cm}^{3}\). The maximum temperature in the cycle is \(2200 \mathrm{~K}\) and the compression ratio is 8. Determine (a) the heat addition, in \(\mathrm{kJ}\). (b) the net work, in \(\mathrm{kJ}\). (c) the thermal efficiency. (d) the mean effective pressure, in bar. (e) Develop a full accounting of the exergy transferred to the air during the heat addition, in \(\mathrm{kJ}\). (f) Devise and evaluate an exergetic efficiency for the cycle. Let \(T_{0}=290 \mathrm{~K}, p_{0}=1\) bar.

Short Answer

Expert verified
q_in = 1120.25 kJ, W_net = 618.10 kJ, η_th = 55.2%, MEP ≈ 17.72 bar, e_q = 973.13 kJ, η_exergetic ≈ 63.54%

Step by step solution

01

Define given parameters

Given values are: \[ p_{1}=1 \text{ bar}, T_{1}=290 \text{ K}, V_{1}=400 \text{ cm}^3 \text{ or } 0.0004 \text{ m}^3 \] \[ T_{max}=2200 \text{ K}, r=8 \] The environmental conditions are \[ T_{0} = 290 \text{ K} \text{ and } p_{0} = 1 \text{ bar} \text{ or } 100 \text{ kPa} \]
02

Calculate intermediate state parameters

First, determine state parameters at the end of compression (state 2): Use the relation \[ V_{2} = \frac{V_{1}}{r} = \frac{0.0004}{8} = 0.00005 \text{ m}^3 \] For an air-standard Otto cycle, we also use the isentropic relations for temperature and pressure during the compression process from state 1 to state 2. For an ideal gas with specific heat ratio \( \gamma = 1.4 \): \[ T_{2}=T_{1}\left(\frac{V_{1}}{V_{2}}\right)^{\gamma-1}=290\left(\frac{0.0004}{0.00005}\right)^{0.4}=645.84 \text{ K} \] \[ \frac{p_{2}}{p_{1}}=\left(\frac{T_{2}}{T_{1}}\right)^{\frac{\gamma}{\gamma-1}}=\left(\frac{645.84}{290}\right)^{\frac{1.4}{0.4}}=\frac{p_{2}}{1}\] Therefore, \[ p_{2}\approx 15.69 \text{ bar} \]
03

Calculate parameters at maximum temperature

Using the relation for the heat addition process (isochoric process from state 2 to 3): \[ V_{3} = V_{2}=V_{1}/r \] \[ T_{3}=2200 \text{ K} \text{ (given)} \text{ and thus from the ideal gas law: } \frac{p_{3}}{p_{2}}= \frac{T_{3}}{T_{2}} \] \[ p_{3}=p_{2}\left(\frac{T_{3}}{T_{2}}\right)=15.69\left( \frac{2200}{645.84} \right) \text { bar } \approx 53.42 \text{ bar} \]
04

Calculate parameters at state 4

At state 4, we assume the isentropic expansion process: \( T_{4} \) and \( p_{4} \) can be found using similar relations as state 2: \[ T_{4}=T_{3}\left(\frac{V_{3}}{V_{4}}\right)^{\gamma-1} = T_{3}\left(\frac{V_{2}}{V_{1}}\right)^{\gamma-1}\] Substituting values: \[ T_{4}=2200 \left( \frac{1}{8} \right)^{0.4} \approx 989.37 \text{K} \] \[ \frac{p_{4}}{p_{3}}=\left(\frac{T_{4}}{T_{3}}\right)^{\frac{\gamma}{\gamma-1}} \] \[ p_{4} = p_{3}\left(\frac{T_{4}}{T_{3}}\right)^{\frac{\gamma}{\gamma-1}} = 53.42\left( \frac{989.37}{2200} \right)^{3.5} \approx 3.41 \text{ bar} \]
05

Compute the heat addition

Using specific heat values for air (constant values): \( c_{v} = 0.718 \text{ kJ/kg.K} \) and noting that \[ q_{in} = c_{v}(T_{3}-T_{2}) \] \[ q_{in}=(0.718)(2200-645.84) \text{ kJ/kg} \text{ } = 1120.25 \text{ kJ} \]
06

Compute the net work

The net work output \( W_{net} \) is the difference between heat added and rejected. Heat rejected \( q_{out} = c_{v}(T_{4}-T_{1}) \): \[ q_{out} = c_{v}(989.37-290) = 0.718 \times 699.37 = 502.15 \text{ kJ} \] Therefore, \[ W_{net}= q_{in} - q_{out} = 1120.25 - 502.15 = 618.10 \text{ kJ} \]
07

Calculate thermal efficiency

The thermal efficiency \( \eta_{th} \) for the Otto cycle is given by: \[ \eta_{th} = 1- \frac{q_{out}}{q_{in}} = 1 - \frac{502.15}{1120.25} = 0.552 \text{ or } 55.2% \]
08

Mean effective pressure

Mean effective pressure (MEP) is given by: \[ MEP = \frac{W_{net}}{V_{1}-V_{2}} = \frac{618.10}{0.0004-0.00005}\, \text{ Pa}\approx 1,771,714 \text{ Pa} \text{ or } 17.72 \text{ bar} \]
09

Exergy transferred during heat addition

Exergy transferred: \[ e_{q} = q_{in} \left(1 - \frac{T_{0}}{T_{3}} \right) = 1120.25 \left(1-\frac{290}{2200} \right) = 973.13 \text{ kJ} \]
10

Exergetic efficiency

Exergy transferred to work output: \[ \eta_{exergetic} = \frac{W_{net}}{e_{q}} = \frac{618.10}{973.13} \approx 63.54% \]

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Key Concepts

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

Heat Addition in Otto Cycle
In the Otto cycle, heat addition occurs during the combustion process. This takes place at constant volume. Here, the air-fuel mixture is ignited, raising the temperature within the cylinder. The amount of heat added, denoted as \( q_{in} \), can be calculated using the specific heat capacity at constant volume \( c_v \), and the temperature change during the process. In our example: \[ q_{in} = c_v (T_3 - T_2) \]. This ensures we have all required parameters to determine the precise heat addition in kilojoules (kJ). \[ q_{in} = 1120.25 \text{ kJ} \].
Net Work in Thermodynamic Cycles
Net work in thermodynamic cycles is crucial for understanding the efficiency of an engine. The net work output \( W_{net} \) is the difference between the work done during heat addition and the work lost during heat rejection. This is represented formally as: \[ W_{net} = q_{in} - q_{out} \]. In our example, the heat rejected \( q_{out} \) is calculated using the specific heat capacity and temperature difference during the heat rejection phase. Subsequently, the net work can be computed: \[ W_{net} = 618.10 \text{kJ} \].
Thermal Efficiency Calculation
Thermal efficiency measures how effectively an engine converts heat into work. For an Otto cycle, the thermal efficiency \( \eta_{th} \) can be determined by the formula: \[ \eta_{th} = 1 - \frac{q_{out}}{q_{in}} \]. The higher the thermal efficiency, the more efficient the engine is. In our case, substituting the values of heat added and rejected yields: \[ \eta_{th} = 55.2% \].
Mean Effective Pressure
Mean effective pressure (MEP) represents the average pressure in the cylinder over one cycle, and it's an important indicator of an engine's performance. Calculated as: \[ \text{MEP} = \frac{W_{net}}{V_{1} - V_{2}} \], where \( W_{net} \) is the net work, and \( V_{1} - V_{2} \) is the change in volume. Here, the MEP is found to be: \[ 17.72 \text{ bar} \]. This helps engineer gauge how effectively the engine can perform useful work.
Exergy in Thermodynamic Cycles
Exergy quantifies the maximum useful work possible during a process that brings the system into equilibrium with its environment. During the heat addition process in the Otto cycle, exergy transferred, denoted as \( e_q \) is calculated by: \[ e_q = q_{in} \(1 - \frac{T_0}{T_3} \) \]. Using given and determined values, the exergy transferred during heat addition is: \[ 973.13 \text{ kJ} \]. Understanding exergy helps optimize the thermodynamic process by evaluating losses and inefficiencies.
Exergetic Efficiency
Exergetic efficiency assesses how efficiently a system converts available energy (exergy) into useful work. This efficiency is crucial for definitive performance improvement and environmental considerations. It is determined by: \[ \eta_{exergetic} = \frac{W_{net}}{e_q} \]. For our specific Otto cycle, the exergetic efficiency is: \[ \eta_{exergetic} = 63.54% \]. This indicates how efficiently the system transforms exergy into work. Enhancements to this metric can lead to significant improvements in overall engine performance and sustainability.

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Most popular questions from this chapter

Consider a modification of the air-standard Otto cycle in which the isentropic compression and expansion processes are each replaced with polytropic processes having \(n=1.3 .\) The compression ratio is 9 for the modified cycle. At the beginning of compression, \(p_{1}=1\) bar and \(T_{1}=300 \mathrm{~K}\). The maximum temperature during the cycle is \(2000 \mathrm{~K}\). Determine (a) the heat transfer and work per unit mass of air, in \(\mathrm{kJ} / \mathrm{kg}\), for each process in the modified cycle. (b) the thermal efficiency. \text { (c) the mean effective pressure, in bar. }

Air as an ideal gas with \(k=1.4\) undergoes a normal shock. The upstream conditions are \(p_{\mathrm{x}}=0.5\) bar, \(T_{\mathrm{x}}=280 \mathrm{~K}\), and \(M_{\mathrm{x}}=1.8 .\) Determine (a) the pressure \(p_{y}\), in bar. (b) the stagnation pressure \(p_{\mathrm{ox}}\), in bar. (c) the stagnation temperature \(T_{\mathrm{ax}}\), in \(\mathrm{K}\). (d) the change in specific entropy across the shock, in \(\mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K}\). (e) Plot the quantities of parts (a)-(d) versus \(M_{x}\) ranging from \(1.0\) to \(2.0\). All other upstream conditions remain the same.

The Stirling engine was first patented in 1816 but has not been widely commercialized. Still, efforts continue to develop Stirling engine technology for practical uses such as vehicle propulsion. Prepare a memorandum summarizing the status of Stirling engine technology. Discuss the advantages and disadvantages of Stirling engines and assess the likelihood that they will be more widely used in the future.

The ideal Brayton and Rankine cycles are composed of the same four processes, yet look different when represented on a \(T-s\) diagram. Explain.

Air enters the diffuser of a ramjet engine at \(40 \mathrm{kPa}, 240 \mathrm{~K}\), with a velocity of \(2500 \mathrm{~km} / \mathrm{h}\) and decelerates to negligible velocity. On the basis of an air-standard analysis, the heat addition is \(1080 \mathrm{~kJ}\) per \(\mathrm{kg}\) of air passing through the engine. Air exits the nozzle at \(40 \mathrm{kPa}\). Determine (a) the pressure at the diffuser exit, in \(\mathrm{kPa}\). (b) the velocity at the nozzle exit, in \(\mathrm{m} / \mathrm{s}\). Neglect kinetic energy except at the diffuser inlet and the nozzle exit.

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