Heat is generated uniformly in a 4-cm-diameter, 12 -cm-long solid bar \((k=2.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). The temperatures at the center and at the surface of the bar are measured to be \(210^{\circ} \mathrm{C}\) and \(45^{\circ} \mathrm{C}\), respectively. The rate of heat generation within the bar is (a) \(597 \mathrm{~W}\) (b) \(760 \mathrm{~W}\) (c) \(826 \mathrm{~W}\) (d) \(928 \mathrm{~W}\) (e) \(1020 \mathrm{~W}\)

Short Answer

Expert verified
Answer: The rate of heat generation within the bar is 826 W.

Step by step solution

01

Write the given information

We have a solid bar with diameter \(4\,\text{cm}\), length \(12\,\text{cm}\), thermal conductivity \(k=2.4\,\frac{\text{W}}{\text{m}\cdot \text{K}}\), center temperature \(T_{\text{center}}=210^\circ\text{C}\), and surface temperature \(T_{\text{surface}}=45^\circ\text{C}\).
02

Calculate the radius of the bar

Half of the diameter is the radius, \(r = \frac{4}{2}\,\text{cm} = 2\,\text{cm}\). We need to convert the radius to meters: \(r = 2\,\text{cm} \times \frac{1\,\text{m}}{100\,\text{cm}} = 0.02\,\text{m}\).
03

Set up the thermal conduction equation

The heat conduction equation for radial heat flow in a cylinder is given by: \(Q = -k A \frac{\Delta T}{\Delta r}\), where \(Q\) is the heat flow rate, \(k\) is the thermal conductivity, \(A\) is the area perpendicular to the heat flow for radial conduction in the cylinder, \(\Delta T\) is the temperature difference, and \(\Delta r\) is the radial distance.
04

Calculate the area A

In this case, the area perpendicular to the heat flow is the lateral surface area of the cylinder: \(A = 2\pi r L\), where L is the length of the cylinder. Substitute the values: \(A = 2\pi(0.02\,\text{m})(0.12\,\text{m}) \approx 0.01508\,\text{m}^2\).
05

Calculate the temperature difference and radial distance

We have \(\Delta T = T_{\text{center}} - T_{\text{surface}} = 210^\circ\,\text{C} - 45^\circ\,\text{C} = 165\,\text{K}\), and \(\Delta r = r = 0.02\,\text{m}\).
06

Substitute the values into the conduction equation

Now, we can find the heat flow rate \(Q\): \(Q = -k A \frac{\Delta T}{\Delta r} = -(-1) (2.4\,\frac{\text{W}}{\text{m}\cdot \text{K}}) (0.01508\,\text{m}^2) \frac{165\,\text{K}}{0.02\,\text{m}} = 826\,\text{W}\) The rate of heat generation within the bar is (c) \(826\,\text{W}\).

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Key Concepts

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

Thermal Conductivity
Thermal conductivity, represented by the symbol k, is a measure of a material's ability to conduct heat. When we talk about heat conduction in solids, thermal conductivity indicates how quickly heat will transfer through the material. A high thermal conductivity means that heat passes through the solid swiftly, whereas a low thermal conductivity indicates that the material is a good insulator and heat moves through it slowly.

In the exercise provided, the thermal conductivity of the solid bar is given as k=2.4 W/m·K, which tells us how effective the bar is at transferring heat from the high temperature area to the low temperature one. This property is crucial for calculating the heat flow rate, as well as understanding how materials behave in thermal applications such as heat sinks, insulation, and construction materials.
Radial Heat Flow
Radial heat flow refers to the movement of heat outwards from the center of an object to its surface or vice versa. This type of heat transfer commonly occurs in cylindrical and spherical objects where the heat spreads out in a circular pattern.

Understanding the concept of radial heat flow is essential for problems like our textbook exercise, where the heat generated within a solid bar must be analyzed. The bar's cylindrical shape means that heat flows from its center to the surface radially. The surface area (A) through which this radial heat flow occurs is critical in calculating the rate of heat flow, as demonstrated in the step-by-step solution.
Heat Transfer Equation
The heat transfer equation is a mathematical representation that calculates the rate of heat transfer in a material. In problems involving thermal conduction, the basic form of the heat transfer equation is Q = -kA(ΔT/Δr), where Q represents the heat flow rate, k is the thermal conductivity, A is the area through which heat is flowing, ΔT is the temperature difference driving the heat transfer, and Δr is the distance over which the temperature change occurs.

For situations involving radial heat flow in solids like a cylindrical bar, the area A is not the cross-sectional area but rather the lateral surface area. Also in radial conduction, Δr is equal to the radius of the cylinder. This adapted heat transfer equation helps predict how much heat will flow through a solid object given a temperature difference, which is a valuable calculation in engineering and design processes.
Solid Bar Heat Generation
Heat generation within a solid refers to the internal production of heat due to various processes, such as electrical resistance, chemical reactions, or radioactive decay. In engineering problems, sometimes this generation is assumed to be uniform throughout the material, simplifying the calculations.

In the context of our exercise, heat is generated uniformly across the solid bar, and we are looking to find the overall rate of this heat generation. To arrive at this rate, we apply the thermal concepts previously discussed: thermal conductivity, radial heat flow, and the heat transfer equation. By solving the equation with the given parameters, we can determine that the rate of heat generation is 826 W, which corresponds to the amount of heat being produced by the bar to maintain the temperature difference observed between its center and surface.

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Most popular questions from this chapter

What is heat generation? Give some examples.

Consider a steam pipe of length \(L=30 \mathrm{ft}\), inner radius \(r_{1}=2\) in, outer radius \(r_{2}=2.4\) in, and thermal conductivity \(k=7.2 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\). Steam is flowing through the pipe at an average temperature of \(300^{\circ} \mathrm{F}\), and the average convection heat transfer coefficient on the inner surface is given to be \(h=12.5 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}\). If the average temperature on the outer surfaces of the pipe is \(T_{2}=175^{\circ} \mathrm{F},(a)\) express the differential equation and the boundary conditions for steady one-dimensional heat conduction through the pipe, \((b)\) obtain a relation for the variation of temperature in the pipe by solving the differential equation, and \((c)\) evaluate the rate of heat loss from the steam through the pipe.

Consider a large plane wall of thickness \(L=0.8 \mathrm{ft}\) and thermal conductivity \(k=1.2 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\). The wall is covered with a material that has an emissivity of \(\varepsilon=0.80\) and a solar absorptivity of \(\alpha=0.60\). The inner surface of the wall is maintained at \(T_{1}=520 \mathrm{R}\) at all times, while the outer surface is exposed to solar radiation that is incident at a rate of \(\dot{q}_{\text {solar }}=300 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}\). The outer surface is also losing heat by radiation to deep space at \(0 \mathrm{~K}\). Determine the temperature of the outer surface of the wall and the rate of heat transfer through the wall when steady operating conditions are reached.

A large steel plate having a thickness of \(L=4\) in, thermal conductivity of \(k=7.2 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\), and an emissivity of \(\varepsilon=0.7\) is lying on the ground. The exposed surface of the plate at \(x=L\) is known to exchange heat by convection with the ambient air at \(T_{\infty}=90^{\circ} \mathrm{F}\) with an average heat transfer coefficient of \(h=12 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\) as well as by radiation with the open sky with an equivalent sky temperature of \(T_{\text {sky }}=480 \mathrm{R}\). Also, the temperature of the upper surface of the plate is measured to be \(80^{\circ} \mathrm{F}\). Assuming steady onedimensional heat transfer, \((a)\) express the differential equation and the boundary conditions for heat conduction through the plate, \((b)\) obtain a relation for the variation of temperature in the plate by solving the differential equation, and \((c)\) determine the value of the lower surface temperature of the plate at \(x=0\).

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