/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 30 A \(0.2-\mathrm{m}\)-thick plane... [FREE SOLUTION] | 91影视

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A \(0.2-\mathrm{m}\)-thick plane wall is constructed of concrete. At steady state, the energy transfer rate by conduction through a \(1-\mathrm{m}^{2}\) area of the wall is \(0.15 \mathrm{~kW}\). If the temperature distribution is linear through the wall, what is the temperature difference across the wall, in \(\mathrm{K}\) ?

Short Answer

Expert verified
The temperature difference across the wall is approximately 17.65 K.

Step by step solution

01

Understand the heat conduction equation

The heat conduction through a plane wall can be described by Fourier's law: \[Q = \frac{kA(T_1 - T_2)}{L}\]where, - \(Q\) is the energy transfer rate (0.15 kW),- \(k\) is the thermal conductivity of the concrete,- \(A\) is the area of the wall (1 m虏),- \(T_1\) and \(T_2\) are the temperatures on the two sides of the wall,- \(L\) is the thickness of the wall (0.2 m).
02

Rearrange the equation to solve for the temperature difference

We need to solve for the temperature difference \(\Delta T = T_1 - T_2\). Rearrange Fourier's law to solve for \(\Delta T\):\[\Delta T = \frac{Q \cdot L}{k \cdot A}\]
03

Substitute known values into the equation

Substitute the known values into the rearranged equation. Note that we need the value for the thermal conductivity \(k\). Let's assume an average value for thermal conductivity of concrete: \(k = 1.7 \mathrm{W}/(\mathrm{m}\cdot\mathrm{K})\). Now plug in the numbers:\[\Delta T = \frac{0.15~\text{kW} \cdot 0.2~\text{m}}{1.7 \frac{\text{W}}{\text{m}\cdot\text{K}} \cdot 1~\text{m}^2}\]Convert 0.15 kW to watts (since 1 kW = 1000 W):\[\Delta T = \frac{150~\text{W} \cdot 0.2~\text{m}}{1.7 \frac{\text{W}}{\text{m}\cdot\text{K}} \cdot 1~\text{m}^2} = \frac{30}{1.7}~\text{K}\]
04

Calculate the temperature difference

Finally, perform the calculation:\[\Delta T = \frac{30}{1.7} \approx 17.65~\text{K}\]

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Key Concepts

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

Fourier's Law of Heat Conduction
In heat transfer, Fourier's Law of Heat Conduction is fundamental. It provides a mathematical model to describe how heat energy transfers through a material. The equation is given by: \[Q = \frac{kA(T_1 - T_2)}{L} \] where:- Q is the rate of heat transfer (in Watts or Kilowatts). - k is the thermal conductivity of the material (W/m路K). - A is the cross-sectional area perpendicular to the direction of heat flow (in m虏). - T鈧 and T鈧 are the temperatures on both sides of the wall (in K). - L is the thickness of the material (in m). This law highlights that heat transfer ( Q ) is directly proportional to the temperature difference ( 螖T=T鈧佲垝T鈧 ), cross-sectional area ( A ), and thermal conductivity ( k ), but inversely proportional to the thickness ( L ) of the material.Understanding this relationship allows us to control the heat flow in different engineering applications, from building insulation to electronic cooling systems.
Thermal Conductivity
Thermal conductivity ( k ) is a property that measures a material's ability to conduct heat. Substances with high thermal conductivity, like metals, conduct heat very efficiently. Conversely, materials with low thermal conductivity, like wood or fiberglass, are good thermal insulators. In the given exercise, the concrete wall's thermal conductivity, k , is assumed to be 1.7 W/(m路K) . This value signifies that for each meter thickness of concrete, a temperature difference of 1 Kelvin results in a heat transfer rate of 1.7 Watts per square meter. When designing systems for heating or cooling, selecting materials with appropriate thermal conductivities is critical to achieving desired heat transfer rates.
Temperature Difference Calculation
The key goal of the exercise is to calculate the temperature difference ( 螖T ) across the wall. Based on Fourier's Law, we rearrange the equation to solve for 螖T :\[ 螖T = \frac{Q路L}{k路A} \]In this specific problem: - Q = 0.15 kW = 150 W (as 1 kW = 1000 W) - L = 0.2 m - k = 1.7 W/(m路K) - A = 1 m虏Plugging these values into the equation provides: \[ 螖T = \frac{150 W路0.2 m}{1.7 W/(m路K)路1 m虏} = \frac{30}{1.7} 鈮 17.65 K \]This result tells us that approximately 17.65 Kelvin is the temperature difference needed to drive the given heat transfer rate through the concrete wall with the specified parameters.
Steady State Heat Transfer
In thermodynamics, steady-state heat transfer occurs when the temperature field in the conducting material does not change over time. In other words, the system has reached an equilibrium, and the rate of heat entering any part of the system equals the rate of heat exiting it.In the provided exercise, the temperature distribution is said to be linear, indicating steady-state conditions. Under steady-state conditions, heat transfer calculations become more straightforward and predictable. This is because the temperature gradient ( T鈧佲垝T鈧 ) remains consistent over time, allowing for precision in designing and assessing thermal systems.Recognizing whether a system is in steady-state or transient (where temperatures change over time) is crucial for selecting the correct analytical approach to solve heat transfer problems.

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Most popular questions from this chapter

Lightweight, portable refrigerated chests are available for keeping food cool. These units use a thermoelectric cooling module energized by plugging the unit into an automobile cigarette lighter. Thermoelectric cooling requires no moving parts and requires no refrigerant. Write a report that explains this thermoelectric refrigeration technology. Discuss the applicability of this technology to larger-scale refrigeration systems.

An object whose mass is \(0.5 \mathrm{~kg}\) has a velocity of \(30 \mathrm{~m} / \mathrm{s}\). Determine (a) the final velocity, in \(\mathrm{m} / \mathrm{s}\), if the kinetic energy of the object decreases by \(130 \mathrm{~J}\). (b) the change in elevation, in \(\mathrm{ft}\), associated with a \(130 \mathrm{~J}\) change in potential energy. Let \(g=9.81 \mathrm{~m} / \mathrm{s}^{2}\).

A closed system undergoes a process during which there is energy transfer from the system by heat at a constant rate of \(10 \mathrm{~kW}\), and the power varies with time according to $$ \dot{W}= \begin{cases}-8 t & 01 \mathrm{~h}\end{cases} $$ where \(t\) is time, in \(\mathrm{h}\), and \(\dot{W}\) is in \(\mathrm{kW}\). (a) What is the time rate of change of system energy at \(t=\) \(0.6 \mathrm{~h}\), in \(\mathrm{kW}\) ? (b) Determine the change in system energy after \(2 \mathrm{~h}\), in \(\mathrm{kJ}\).

An object whose mass is \(400 \mathrm{~kg}\) is located at an elevation of \(25 \mathrm{~m}\) above the surface of the earth. For \(g=9.78 \mathrm{~m} / \mathrm{s}^{2}\), determine the gravitational potential energy of the object, in \(\mathrm{kJ}\), relative to the surface of the earth.

A storage battery develops a power output of $$ \dot{W}=1.2 \exp (-t / 60) $$ where \(\dot{W}\) is power, in \(\mathrm{kW}\), and \(t\) is time, in s. Ignoring heat transfer (a) plot the power output, in \(\mathrm{kW}\), and the change in energy of the battery, in \(\mathrm{kJ}\), each as a function of time. (b) What are the limiting values for the power output and the change in energy of the battery as \(t \rightarrow \infty\) ? Discuss.

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