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Heat is lost through a brick wall \((k=0.72 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\), which is \(4 \mathrm{~m}\) long, \(3 \mathrm{~m}\) wide, and \(25 \mathrm{~cm}\) thick at a rate of \(500 \mathrm{~W}\). If the inner surface of the wall is at \(22^{\circ} \mathrm{C}\), the temperature at the midplane of the wall is (a) \(0^{\circ} \mathrm{C}\) (b) \(7.5^{\circ} \mathrm{C}\) (c) \(11.0^{\circ} \mathrm{C}\) (d) \(14.8^{\circ} \mathrm{C}\) (e) \(22^{\circ} \mathrm{C}\)

Short Answer

Expert verified
#tag_title# Step 2: Calculate the surface area of the wall #tag_content# To find the surface area, multiply the length and the width of the wall: \(A = L \times W = 4 \mathrm{~m} \times 3 \mathrm{~m} = 12 \mathrm{~m^2}\) #tag_title# Step 3: Rearrange the heat transfer formula to solve for ΔT #tag_content# We have the values for \(k\), \(A\), and \(d\), so we can rearrange the heat transfer formula to solve for the temperature difference, \(\Delta T\): \(\Delta T = \dfrac{Q \times d}{k \times A}\) #tag_title# Step 4: Substitute the known values and calculate ΔT #tag_content# Plug in the known values into the expression for \(\Delta T\), and then calculate it: \(\Delta T = \dfrac{500 \mathrm{~W} \times 0.25 \mathrm{~m}}{0.72 \mathrm{W/m\cdot K} \times 12 \mathrm{~m^2}} \approx 14.58 \mathrm{K}\) #tag_title# Step 5: Calculate the midplane temperature #tag_content# Now, we need to find the temperature at the midplane. Since we know the inner surface temperature (\(T_{inner}\)) and the complete temperature difference across the wall (\(\Delta T\)), we can assume that half of the temperature difference occurs across half the thickness of the wall. So we can find the midplane temperature by subtracting half of \(\Delta T\) from \(T_{inner}\): \(T_{midplane} = T_{inner} - \dfrac{\Delta T}{2} \approx 22^{\circ} \mathrm{C} - \dfrac{14.58 \mathrm{K}}{2} \approx 14.71^{\circ} \mathrm{C}\) So the temperature at the midplane of the brick wall is approximately \(14.71^{\circ} \mathrm{C}\).

Step by step solution

01

List the given values

We are given the following information about the brick wall and heat transfer: - Thermal conductivity, \(k = 0.72 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) - Length, \(L = 4 \mathrm{~m}\) - Width, \(W = 3 \mathrm{~m}\) - Thickness, \(d = 25 \mathrm{~cm} = 0.25 \mathrm{~m}\) (converted to meters) - Rate of heat loss, \(Q = 500 \mathrm{~W}\) - Inner surface temperature, \(T_{inner} = 22^{\circ} \mathrm{C}\)

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Key Concepts

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

Thermal Conductivity
Thermal conductivity is a property that measures a material's ability to conduct heat. It represents how easily heat can pass through a material. The higher the thermal conductivity of a substance, the more efficient it is at transferring heat. It is denoted by the symbol \( k \) and is measured in watts per meter Kelvin \( (W/m \cdot K) \). For example, metals typically have high thermal conductivity, making them good heat conductors, while materials like brick, with a lower \( k \) value, are less efficient but still used in construction due to their thermal mass properties.

In the exercise, we use the thermal conductivity \( k = 0.72 W/m \cdot K \) for calculations. This value is crucial to determine the rate of heat transfer through the brick wall. The choice of materials with specific thermal conductivities can impact heating and cooling requirements for buildings retrospectively.
Steady-State Heat Conduction
Steady-state heat conduction occurs when the temperature distribution in a material does not change over time; that is, the amount of heat entering a section of the material is equal to the amount of heat exiting the same section. There is no net accumulation of heat within the material, and the temperature gradient remains constant.

This concept is essential for long-term analysis of heat transfer in structures, as it helps in the design phase to ensure that heating or cooling loads are consistent. It simplifies calculations since we can assume the heat transfer rate is unchanging. In our problem, we're inferring a steady-state condition to calculate the temperature at the midplane of the brick wall.
Fourier’s Law of Heat Conduction
Fourier’s law of heat conduction is a fundamental principle which quantifies the heat transfer through a material. It states that the heat transfer rate \( Q \) through a material is proportional to the negative gradient of the temperature and the area \( A \) perpendicular to the heat transfer direction, and inversely proportional to the thickness \( d \) of the material. Mathematically, it is expressed as:

\[ Q = -k A \frac{dT}{dx} \]
Where:\( Q \) is the heat transfer rate in watts (\( W \)),\( k \) is the thermal conductivity,\( A \) is the area through which heat is being transferred,\( \frac{dT}{dx} \) is the temperature gradient, and\( d \) is the thickness of the material.

Fourier's law helps us understand how different factors affect heat transfer. In practice, it means that if we have a material with a known thermal conductivity and area, and we can measure the temperature difference across it, we can calculate the rate at which heat flows through the material.
Temperature Distribution
Temperature distribution within a material under steady-state heat conduction tells us how temperature varies from one point to another. It's fundamental in evaluating and designing thermal systems, as uneven temperature distribution can lead to thermal stresses and inefficiencies.

With knowledge of the thermal conductivity and boundary conditions (like known surface temperatures), we can estimate the temperature at any point within the material. This assumes a linear temperature gradient between points when dealing with simple, homogeneous materials. In the provided exercise, determining the temperature at the midplane involves knowing the temperature at the surfaces and using the heat transfer rate to deduce the temperature distribution in the wall's interior.

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Most popular questions from this chapter

While driving down a highway early in the evening, the air flow over an automobile establishes an overall heat transfer coefficient of \(18 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The passenger cabin of this automobile exposes \(9 \mathrm{~m}^{2}\) of surface to the moving ambient air. On a day when the ambient temperature is \(33^{\circ} \mathrm{C}\), how much cooling must the air conditioning system supply to maintain a temperature of \(20^{\circ} \mathrm{C}\) in the passenger cabin? (a) \(670 \mathrm{~W}\) (b) \(1284 \mathrm{~W}\) (c) \(2106 \mathrm{~W}\) (d) \(2565 \mathrm{~W}\) (e) \(3210 \mathrm{~W}\)

The rate of heat loss through a unit surface area of a window per unit temperature difference between the indoors and the outdoors is called the \(U\)-factor. The value of the \(U\)-factor ranges from about \(1.25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (or \(0.22 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}\) ) for low-e coated, argon-filled, quadruple-pane windows to \(6.25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (or \(1.1 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}\) ) for a single-pane window with aluminum frames. Determine the range for the rate of heat loss through a \(1.2-\mathrm{m} \times 1.8-\mathrm{m}\) window of a house that is maintained at \(20^{\circ} \mathrm{C}\) when the outdoor air temperature is \(-8^{\circ} \mathrm{C}\).

A series of experiments were conducted by passing \(40^{\circ} \mathrm{C}\) air over a long \(25 \mathrm{~mm}\) diameter cylinder with an embedded electrical heater. The objective of these experiments was to determine the power per unit length required \((\dot{W} / L)\) to maintain the surface temperature of the cylinder at \(300^{\circ} \mathrm{C}\) for different air velocities \((V)\). The results of these experiments are given in the following table: $$ \begin{array}{lccccc} \hline V(\mathrm{~m} / \mathrm{s}) & 1 & 2 & 4 & 8 & 12 \\ \dot{W} / L(\mathrm{~W} / \mathrm{m}) & 450 & 658 & 983 & 1507 & 1963 \\ \hline \end{array} $$ (a) Assuming a uniform temperature over the cylinder, negligible radiation between the cylinder surface and surroundings, and steady state conditions, determine the convection heat transfer coefficient \((h)\) for each velocity \((V)\). Plot the results in terms of \(h\left(\mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\right)\) vs. \(V(\mathrm{~m} / \mathrm{s})\). Provide a computer generated graph for the display of your results and tabulate the data used for the graph. (b) Assume that the heat transfer coefficient and velocity can be expressed in the form of \(h=C V^{m}\). Determine the values of the constants \(C\) and \(n\) from the results of part (a) by plotting \(h\) vs. \(V\) on log-log coordinates and choosing a \(C\) value that assures a match at \(V=1 \mathrm{~m} / \mathrm{s}\) and then varying \(n\) to get the best fit.

Two surfaces, one highly polished and the other heavily oxidized, are found to be emitting the same amount of energy per unit area. The highly polished surface has an emissivity of \(0.1\) at \(1070^{\circ} \mathrm{C}\), while the emissivity of the heavily oxidized surface is \(0.78\). Determine the temperature of the heavily oxidized surface.

Why is it necessary to ventilate buildings? What is the effect of ventilation on energy consumption for heating in winter and for cooling in summer? Is it a good idea to keep the bathroom fans on all the time? Explain.

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