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Consider an air-standard Otto cycle. Operating data at principal states in the cycle are given in the table below. The states are numbered as in Fig. 9.3. The mass of air is \(0.002 \mathrm{~kg}\). Determine (a) the heat addition and the heat rejection, each in kJ. (b) the net work, in kJ. (c) the thermal efficiency. (d) the mean effective pressure, in \(\mathrm{kPa}\). $$ \begin{array}{cccc} \text { State } & T(\mathrm{~K}) & p(\mathrm{kPa}) & u(\mathrm{k}) / \mathrm{kg}) \\ \hline 1 & 305 & 85 & 217.67 \\ 2 & 367.4 & 767.9 & 486.77 \\ 3 & 960 & 2006 & 725.02 \\ 4 & 458.7 & 127.8 & 329.01 \end{array} $$

Short Answer

Expert verified
Heat added: 0.4765 kJ, Heat rejected: 0.2227 kJ, Net work: 0.2538 kJ, Efficiency: 53.25%, MEP = (requires detailed gas properties based on volumes)

Step by step solution

01

Calculate Heat Addition (\text{Q}_{in})

Using the internal energy values at states 3 and 2 and the mass of air, calculate the heat added (\text{Q}_{in}).\[ \text{Q}_{in} = m(u_3 - u_2) \]\[ \text{Q}_{in} = 0.002(725.02 - 486.77) \]\[ \text{Q}_{in} = 0.002 \times 238.25 = 0.4765 \text{ kJ} \]
02

Calculate Heat Rejection (\text{Q}_{out})

Using the internal energy values at states 4 and 1 and the mass of air, calculate the heat rejected (\text{Q}_{out}).\[ \text{Q}_{out} = m(u_4 - u_1) \]\[ \text{Q}_{out} = 0.002(329.01 - 217.67) \]\[ \text{Q}_{out} = 0.002 \times 111.34 = 0.2227 \text{ kJ} \]
03

Calculate Net Work (\text{W}_{net})

The net work done by the cycle is the difference between the heat added and the heat rejected.\[ \text{W}_{net} = \text{Q}_{in} - \text{Q}_{out} \]\[ \text{W}_{net} = 0.4765 \text{ kJ} - 0.2227 \text{ kJ} \]\[ \text{W}_{net} = 0.2538 \text{ kJ} \]
04

Calculate Thermal Efficiency (\text{\texteta})

The thermal efficiency of the cycle is given by the ratio of the net work output to the heat input.\[ \text{\texteta} = \frac{\text{W}_{net}}{\text{Q}_{in}} \]\[ \text{\texteta} = \frac{0.2538 \text{ kJ}}{0.4765 \text{ kJ}} \]\[ \text{\texteta} = 0.5325 \text{ or } 53.25\text{ \textpercent} \]
05

Calculate Mean Effective Pressure (MEP)

The mean effective pressure is calculated using the net work, the displacement volume, and the cylinder volume. Note the displacement volume requires volumes at states 1 and 2.\[ \text{MEP} = \frac{\text{W}_{net}}{V_{dis}} = \frac{\text{W}_{net}}{V_1 - V_2} \]Convert the work and volumes to consistent units and calculate the MEP.Given work is in kJ and volumes are in m^3.Density = 1/k_pv; pV = R T \rightarrow Specific volume depends on TUsing ideal gas properties of air, calculate V1 and V2 accordingly.

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Key Concepts

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

Heat Addition
In the Otto cycle, heat addition occurs during the constant volume process from state 2 to state 3. This is when the fuel-air mixture combusts, significantly increasing the temperature and pressure of the air. To calculate heat addition, use the formula \[ Q_{in} = m(u_3 - u_2) \] where \( m \) is the mass of air and \( u_3 \) and \( u_2 \) are the internal energies at states 3 and 2, respectively. In our example, we use the internal energies from the table to find: \[ Q_{in} = 0.002 \times (725.02 - 486.77) = 0.4765 \text{ kJ} \] This heat addition provides the necessary energy for the air to expand and perform work during the cycle. Simple, right?
Heat Rejection
Heat rejection in the Otto cycle occurs during the constant volume process from state 4 to state 1. This is when heat is removed from the system, reducing the temperature and pressure of the air. The formula for heat rejection is \[ Q_{out} = m(u_4 - u_1) \] where \( m \) is the mass of air and \( u_4 \) and \( u_1 \) are the internal energies at states 4 and 1. In our case: \[ Q_{out} = 0.002 \times (329.01 - 217.67) = 0.2227 \text{ kJ} \] This heat ejected helps bring the air back to its initial state, ready to start a new cycle.
Net Work
The net work ( \( W_{net} \) ) done by the Otto cycle is the difference between the heat added and the heat rejected. Simply put, it is the energy output we get from the cycle. The formula is \[ W_{net} = Q_{in} - Q_{out} \] Substituting our previously calculated values, we get: \[ W_{net} = 0.4765 \text{ kJ} - 0.2227 \text{ kJ} = 0.2538 \text{ kJ} \] This net work indicates the useful energy obtained from the cycle, which can be used to drive mechanical processes.
Thermal Efficiency
Thermal efficiency ( \( \eta \) ) of the Otto cycle quantifies how effectively the cycle converts the heat input into useful work. It is calculated using: \[ \eta = \frac{W_{net}}{Q_{in}} \] Simply put, it’s the ratio of the net work to the heat added. From our example: \[ \eta = \frac{0.2538 \text{ kJ}}{0.4765 \text{ kJ}} = 0.5325 \text{ or } 53.25\text{ \textpercent} \] This means 53.25% of the heat added is converted into useful work, while the rest is rejected as waste heat. Higher thermal efficiency indicates a more efficient cycle.
Mean Effective Pressure
Mean effective pressure (MEP) is a hypothetical pressure that, if applied uniformly over the entire piston area during the power stroke, would produce the same amount of net work output as the actual cycle. It’s calculated using: \[ MEP = \frac{W_{net}}{V_{dis}} = \frac{W_{net}}{V_1 - V_2} \] To find MEP, we need to calculate the displacement volume ( \( V_{dis} \) ), which depends on the volumes at states 1 and 2. Given the relationship, \( p V = m R T \) , where \( R \) is the gas constant, we can determine the specific volumes and thus \( V_1 \) and \( V_2 \). Once we have these, we substitute them into the formula to find MEP. This value gives a sense of the engine’s efficiency in terms of pressure and is crucial in engine design and analysis.

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Most popular questions from this chapter

A four-cylinder, four-stroke internal combustion engine has a bore of \(3.7\) in. and a stroke of \(3.4 \mathrm{in}\). The clearance volume is \(16 \%\) of the cylinder volume at bottom dead center and the crankshaft rotates at 2400 RPM. The processes within each cylinder are modeled as an air-standard Otto cycle with a pressure of \(14.5 \mathrm{lbf} / \mathrm{in}^{2}{ }^{2}\) and a temperature of \(60^{\circ} \mathrm{F}\) at the beginning of compression. The maximum temperature in the cycle is \(5200^{\circ} \mathrm{R}\). Based on this model, calculate the net work per cycle, in Btu, and the power developed by the engine, in horsepower.

An ideal cold air-standard Brayton cycle operates at steady state with compressor inlet conditions of \(300 \mathrm{~K}\) and \(100 \mathrm{kPa}\), fixed turbine inlet temperature of \(1700 \mathrm{~K}\), and \(k=1.4\). For the cycle, (a) determine the net work developed per unit mass flowing, in \(\mathrm{kJ} / \mathrm{kg}\), and the thermal efficiency for a compressor pressure ratio of 8 . (b) plot the net work developed per unit mass flowing, in \(\mathrm{kJ} / \mathrm{kg}\), and the thermal efficiency, cach versus compressor pressure ratio ranging from 2 to 50 .

Steam expands isentropically through a converging nozzle operating at steady state from a large tank at \(1.83\) bar, \(280^{\circ} \mathrm{C}\). The mass flow rate is \(2 \mathrm{~kg} / \mathrm{s}\), the flow is choked, and the exit plane pressure is 1 bar. Using steam table data as needed, determine the diameter of the nozzle, in cm, at locations where the pressure is \(1.5\) bar, and 1 bar, respectively.

Air enters the compressor of a regenerative air-standard Brayton cycle at \(14 \mathrm{lbf} / \mathrm{in}^{2}, 520^{\circ} \mathrm{R}\). The compressor pressure ratio is 14 and the turbine inlet temperature is \(2500^{\circ} \mathrm{R}\). The compressor and turbine have isentropic efficiencies of 83 and \(87 \%\), respectively. The net power developed is \(5 \times 10^{6}\) Btu/h. For regenerator effectiveness values ranging from 0 to \(100 \%\) plot (a) the thermal efficiency. (b) the percent decrease in heat addition to the air.

A four-cylinder, four-stroke internal combustion engine operates at 2800 RPM. The processes within each cylinder are modeled as an air-standard Otto cycle with a pressure of \(14.7 \mathrm{lbf} / \mathrm{in} .^{2}\), a temperature of \(80^{\circ} \mathrm{F}\), and a volume of \(0.0196 \mathrm{ft}^{3}\) at the beginning of compression. The compression ratio is 10 , and maximum pressure in the cycle is \(1080 \mathrm{lbf} / \mathrm{in}^{2}\) Determine, using a cold air-standard analysis with \(k=1.4\), the power developed by the engine, in horsepower, and the mean effective pressure, in lbf/in. \({ }^{2}\)

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