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Ch 20: The Second Law of Thermodynamics
Chapter 20, Problem 20

(a) Calculate the theoretical efficiency for an Otto-cycle engine with g = 1.40 and r = 9.50.

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Identify the given values: the specific heat ratio (\(\gamma\)) is 1.40, and the compression ratio (\(r\)) is 9.50.
Recall the formula for the efficiency (\(\eta\)) of an Otto cycle, which is given by \(\eta = 1 - \frac{1}{r^{\gamma - 1}}\).
Substitute the given values into the efficiency formula. Replace \(\gamma\) with 1.40 and \(r\) with 9.50.
Calculate the exponent \(\gamma - 1\) which is 1.40 - 1 = 0.40.
Evaluate the expression \(r^{\gamma - 1}\) which is \(9.50^{0.40}\), and then compute \(1 - \frac{1}{9.50^{0.40}}\) to find the efficiency.

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Key Concepts

Here are the essential concepts you must grasp in order to answer the question correctly.

Otto Cycle

The Otto cycle is a thermodynamic cycle that describes the functioning of a gasoline engine. It consists of two adiabatic processes and two isochoric processes, where the fuel-air mixture is compressed and then ignited, producing work. Understanding the Otto cycle is essential for analyzing engine efficiency and performance.
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Efficiency of an Engine

The efficiency of an engine is a measure of how well it converts the energy from fuel into useful work. For an Otto cycle engine, the theoretical efficiency can be calculated using the formula: η = 1 - (1/g^(r-1)), where g is the specific heat ratio and r is the compression ratio. This efficiency is crucial for evaluating engine performance.
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Specific Heat Ratio (g)

The specific heat ratio, denoted as g (gamma), is the ratio of the specific heat at constant pressure (Cp) to the specific heat at constant volume (Cv). It is a critical parameter in thermodynamics that influences the behavior of gases during compression and expansion processes in engines. For air, g is typically around 1.40, which is relevant for calculating the efficiency of an Otto cycle engine.
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