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Investigate the effect of maximum cycle temperature on the net work per unit mass of air for air-standard Otto cycles with compression ratios of 5,8, and 11. At the beginning of the compression process, p1=1 bar and T1=295 K. Let the maximum temperature in each case vary from 1000 to 2200 K.

Short Answer

Expert verified
Calculate net work per unit mass using the Otto cycle formula and plot results for different compression ratios and maximum temperatures.

Step by step solution

01

- Define Given Values

Identify and list all the given values.- Compression ratios: 5, 8, 11- Initial pressure: p1=1 bar- Initial temperature: T1=295 K- Maximum temperature range: T3=1000 K to T3=2200 K
02

- Understand the Otto Cycle

The Otto cycle consists of four processes: an isentropic compression, a constant-volume heat addition, an isentropic expansion, and a constant-volume heat rejection. The net work per unit mass of air can be determined from these processes.
03

- Apply Isentropic Relations

Use the isentropic relations to determine various state properties. For the compression process, T2=T1(rc)(γ1γ) where rc is the compression ratio and γ is the specific heat ratio (assume γ=1.4).
04

- Calculate State 2 Properties

For each compression ratio, calculate the temperature after the isentropic compression (state 2). For r_c = 5, 8, and 11: T25=295×5(1.411.4)=526KT28=295×8(1.411.4)=643KT211=295×11(1.411.4)=740K
05

- Apply the Heat Addition Process

For each case, let the maximum temperature T3 vary from 1000 K to 2200 K. Use Qin=cv(T3T2) to calculate the heat added, where cv is the specific heat at constant volume.
06

- Apply Isentropic Expansion

Determine the temperature after the isentropic expansion (state 4) using the relation: T4=T3(rc)(1γγ)
07

- Calculate State 4 Properties

Calculate T4 for each T3 and compression ratio. For example, for T3=10002200K at rc=5:T45,1000=1000×5(11.41.4)=561KT45,2200=2200×5(11.41.4)=1235K
08

- Calculate Net Work Per Unit Mass

The net work per unit mass is given by: Wnet=QinQout Qout=cv(T4T1). Calculate Wnet for each compression ratio and maximum temperature combination.
09

- Plot Results

Plot the net work per unit mass against the maximum temperature for each compression ratio (5, 8, and 11) to visualize the effect of maximum cycle temperature.

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Key Concepts

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

Otto cycle
The Otto cycle is a fundamental concept in thermodynamics, particularly for internal combustion engines. It's a theoretical model that helps understand how engines convert fuel into work. The cycle consists of four key processes:
1. **Isentropic Compression:** The air-fuel mixture is compressed, increasing its pressure and temperature, but no heat is exchanged with the surroundings.
2. **Constant-Volume Heat Addition:** The compressed air-fuel mixture ignites. This process increases the temperature and pressure at constant volume.
3. **Isentropic Expansion:** The high-pressure, high-temperature gas expands, doing work on the piston, similar to the compression process but in reverse.
4. **Constant-Volume Heat Rejection:** The heat is expelled at constant volume. Understanding these processes helps in analyzing the performance and efficiency of an engine. Higher maximum cycle temperatures can lead to more efficient engines, but they also place more stress on engine components. Each process impacts the net work produced by the engine.
Compression Ratio
The compression ratio is crucial for understanding the efficiency of the Otto cycle. It's defined as the ratio of the total cylinder volume when the piston is at the bottom of the stroke (largest volume) to when the piston is at the top of the stroke (smallest volume). Mathematically, it is represented as:
Compression Ratio=V1V2 where V1 is the initial volume and V2 is the final compressed volume. Higher compression ratios lead to greater efficiency because they allow for more work to be extracted from the same amount of fuel. However, an increase in compression ratio also raises the temperature and pressure inside the cylinder, which can cause engine knocking—a condition where fuel pre-ignites before the spark plug fires, potentially damaging the engine.
Isentropic Compression
Isentropic compression is a reversible adiabatic process where the entropy remains constant. For the Otto cycle, it occurs when the air-fuel mixture is compressed in the cylinder. The temperature and pressure of the gas increase without any heat exchange with the environment. The relationship between temperature and pressure during isentropic compression is crucial for calculating the states of the system. It's given by:
T2=T1×rc(γ1γ) where T1 and T2 are the initial and final temperatures, rc is the compression ratio, and γ (gamma) is the specific heat ratio, typically around 1.4 for air. This step helps calculate the temperature of the air-fuel mixture after the compression stage, which is essential for further calculations in the cycle.
Net Work Calculation
Calculating the net work per unit mass is essential for assessing an engine's performance. In the Otto cycle, the net work is the difference between the heat added during the combustion phase and the heat rejected during the exhaust phase. The net work can be calculated as:
Wnet=QinQout where Qin=cv×(T3T2) and Qout=cv×(T4T1), with T3 and T4 being the temperatures after combustion and expansion, respectively, and cv being the specific heat at constant volume. This calculation involves determining the temperatures at different stages of the cycle, particularly after compression (T2) and expansion (T4). By varying the maximum cycle temperature (T3), one can analyze its effect on the net work, providing insights into optimizing engine performance.

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Most popular questions from this chapter

Consider a two-stage turbine operating at steady state with reheat at constant pressure between the stages. Show that the maximum work is developed when the pressure ratio is the same across each stage. Use a cold air-standard analysis, assuming the inlet state and the exit pressure are specified, each expansion process is isentropic, and the temperature at the inlet to each turbine stage is the same. Kinetic and potential energy effects can be ignored.

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

For the isentropic flow of an ideal gas with constant specific heat ratio k, the ratio of the temperature T to the stagnation temperature To is T/To=2/(k+1). Develop this relationship.

Nitrogen (N2) is the working fluid of a Stirling cycle with a compression ratio of nine. At the beginning of the isothermal compression, the temperature, pressure, and volume are 310 K,1 bar, and 0.008 m3, respectively. The temperature during the isothermal expansion is 1000 K. Determine (a) the net work, in kJ. (b) the thermal efficiency. (c) the mean effective pressure, in bar.

Air enters the turbine of a gas turbine at 1200kPa,1200 K, and expands to 100kPa in two stages. Between the stages, the air is reheated at a constant pressure of 350kPa to 1200 K. The expansion through each turbine stage is isentropic. Determine, in kJ per kg of air flowing (a) the work developed by each stage. (b) the heat transfer for the reheat process. (c) the increase in net work as compared to a single stage of expansion with no reheat.

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