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The temperature of an incompressible substance of mass \(m\) and specific heat \(c\) is reduced from \(T_{0}\) to \(T\left(

Short Answer

Expert verified
Plot \ \frac{W_{\min}}{m c T_0} = \frac{1 - x}{x} \ versus \ x = \frac{T}{T_0} \ for \ 0.8 \leq x \leq 1.0.

Step by step solution

01

- Understand the Problem

The goal is to find the minimum theoretical work input required by a refrigeration cycle and then plot a specific ratio involving that work over a certain range of temperatures.
02

- Define the Minimum Work Input

Using the second law of thermodynamics for an ideal refrigeration process, the minimum work input, \(W_{\min}\), can be derived via the coefficient of performance (COP). For refrigeration, \(COP = \frac{Q_{\text{out}}}{W_{\text{min}}}\), where \(Q_{\text{out}} = m c (T_0 - T)\).
03

- Apply the Coefficient of Performance

For an ideal refrigeration cycle, \(COP = \frac{T}{T_0 - T}\). Rearranging this formula to find \(W_{\min}\) yields: \[ W_{\min} = m c (T_0 - T) \frac{T_0}{T} \].
04

- Simplify the Expression

Next, simplify the work expression into the requested form. The equation becomes \[ \frac{W_{\min}}{m c T_0} = \frac{T_0 - T}{T} \].
05

- Define the Ratio

Let \(x = \frac{T}{T_0}\), then \( \frac{W_{\min}}{m c T_0} = \frac{1 - x}{x} \).
06

- Plot the Function

Plot the function \[ \frac{W_{\min}}{m c T_0} = \frac{1 - x}{x} \] versus \(x\) for \(x \) ranging from 0.8 to 1.0. This can be done using graphing software or by hand on graph paper.

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Key Concepts

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

incompressible substance
An incompressible substance is a material whose volume or density does not change significantly with changes in pressure. This property is typical of most liquids.

In our exercise, we assume the substance is incompressible to simplify the analysis. This assumption is crucial because it means the substance's volume and specific heat (denoted as c) remain constant throughout the process. These constants simplify our calculations for determining the minimum theoretical work input.
specific heat
The specific heat of a substance, represented by the symbol c, is the amount of heat required to change the temperature of a unit mass of the substance by one degree. It is defined by the equation:

\[ \text{specific heat} = \frac{Q}{m \times \triangle T} \ \ \] where \(Q\) is the heat added or removed, \(m\) is the mass, and \( \triangle T\) is the change in temperature.

In our context, knowing the specific heat helps us relate the heat transfer needed to achieve a particular temperature change (from \(T_0\) to \(T\)) in the refrigeration cycle. This relationship is critical for calculating the required work input.
second law of thermodynamics
The Second Law of Thermodynamics is fundamental in refrigeration cycle analysis. It states that heat transfer occurs spontaneously from higher to lower temperatures. For refrigeration, we need to input work to transfer heat in the opposite direction.

This principle is key to understand minimum work input using the ideal coefficient of performance (COP). By leveraging the second law, we derive the relationship:

\[ \text{COP} = \frac{Q_{\text{out}}}{W_{\text{min}}} \ \]

Where:
  • COP is the coefficient of performance
  • \(Q_{\text{out}}\) is the heat removed
  • \(W_{\text{min}}\) is the minimum work input
coefficient of performance
The coefficient of performance (COP) is a measure of a refrigeration cycle's efficiency. It is defined as the ratio of useful heating or cooling provided to the work required:

\[ \text{COP} = \frac{T}{T_0 - T} \ \]

For our problem, the equation helps us determine the work required for ideal scenarios. Replacing the COP value in our equations and rearranging gives us:

\[ W_{\text{min}} = m c (T_0 - T) \frac{T_0}{T} \ \ \]
This equation shows how the work required depends on temperature changes and the specific heat capacity of the substance. Simplifying further allows plotting the desired function:

\[ \frac{W_{\text{min}}}{m c T_0} = \frac{T_0 - T}{T} \ \] Letting \( x = \frac{T}{T_0} \), we get: \[ \frac{W_{\text{min}}}{m c T_0} = \frac{1 - x}{x} \ \]

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Most popular questions from this chapter

Of increasing interest today are turbines, pumps, and heat exchangers that weigh less than 1 gram and have volumes of 1 cubic centimeter or less. Although many of the same design considerations apply to such micromachines as to corresponding full-scale devices, others do not. Of particular interest to designers is the impact of irreversibilities on the performance of such tiny devices. Write a report discussing the influence of irreversibilities related to heat transfer and friction on the design and operation of micromachines.

A patent application describes a device that at steady state receives a heat transfer at the rate \(1 \mathrm{~kW}\) at a temperature of \(167^{\circ} \mathrm{C}\) and generates electricity. There are no other energy transfers. Does the claimed performance violate any principles of thermodynamics? Explain.

In a gas turbine operating at steady state, air enters the compressor with a mass flow rate of \(5 \mathrm{~kg} / \mathrm{s}\) at \(0.95\) bar and \(22^{\circ} \mathrm{C}\) and exits at \(5.7\) bar. The air then passes through a heat exchanger before entering the turbine at \(1100 \mathrm{~K}, 5.7\) bar. Air exits the turbine at \(0.95\) bar. The compressor and turbine operate adiabatically and kinetic and potential energy effects can be ignored. Determine the net power developed by the plant, in \(\mathrm{kW}\), if (a) the compressor and turbine operate without internal irreversibilities. (b) the compressor and turbine isentropic efficiencies are 82 and \(85 \%\), respectively.

A system undergoing a thermodynamic cycle receives \(Q_{\mathrm{H}}\) at temperature \(T_{\mathrm{H}}^{\prime}\) and discharges \(Q_{\mathrm{C}}\) at temperature \(T_{\mathrm{C}}^{\prime}\). There are no other heat transfers. (a) Show that the net work developed per cycle is given by $$ W_{\text {cycle }}=Q_{\mathrm{H}}\left(1-\frac{T_{\mathrm{C}}^{\prime}}{T_{\mathrm{H}}^{\prime}}\right)-T_{\mathrm{C}}^{\prime} \sigma $$ where \(\sigma\) is the amount of entropy produced per cycle owing to irreversibilities within the system. (b) If the heat transfers \(Q_{\mathrm{H}}\) and \(Q_{\mathrm{C}}\) are with hot and cold reservoirs, respectively, what is the relationship of \(T_{\mathrm{H}}^{\prime}\) to the temperature of the hot reservoir \(T_{\mathrm{H}}\) and the relationship of \(T_{\mathrm{C}}^{\prime}\) to the temperature of the cold reservoir \(T_{\mathrm{C}}\) ? (c) Obtain an expression for \(W_{\text {cycle }}\) if there are (i) no internal irreversibilities, (ii) no internal or external irreversibilities.

Air enters an insulated compressor operating at steady state at 1 bar, \(350 \mathrm{~K}\) with a mass flow rate of \(1 \mathrm{~kg} / \mathrm{s}\) and exits at 4 bar. The isentropic compressor efficiency is \(82 \%\). Determine the power input, in \(\mathrm{kW}\), and the rate of entropy production, in \(\mathrm{kW} / \mathrm{K}\), using the ideal gas model with (a) data from Table A-22. (b) \(I T\). (c) a constant specific heat ratio, \(k=1.39\).

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