/*! 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 146 A row of 3 -ft-long and 1-in-dia... [FREE SOLUTION] | 91Ó°ÊÓ

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A row of 3 -ft-long and 1-in-diameter used uranium fuel rods that are still radioactive are buried in the ground parallel to each other with a center-to- center distance of 8 in at a depth of \(15 \mathrm{ft}\) from the ground surface at a location where the thermal conductivity of the soil is \(0.6 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\). If the surface temperature of the rods and the ground are \(350^{\circ} \mathrm{F}\) and \(60^{\circ} \mathrm{F}\), respectively, determine the rate of heat transfer from the fuel rods to the atmosphere through the soil.

Short Answer

Expert verified
Answer: The rate of heat transfer from the fuel rods to the atmosphere through the soil is approximately 9.42 Btu/h.

Step by step solution

01

Identify known values

Here are the known values that we have: - Length of the fuel rods: 3 ft - Diameter of the fuel rods: 1 in (0.0833 ft) - Depth from the ground surface: 15 ft - Thermal conductivity (k) of the soil: 0.6 Btu/h·ft·F - Surface temperature of the rods (T1): 350°F - Ground temperature (T2): 60°F
02

Calculate the temperature difference between the fuel rods and the ground

We have to find the temperature difference between the surface of the rods and the ground. The calculation is as follows: ΔT = T1 - T2 ΔT = 350°F - 60°F ΔT = 290°F
03

Calculate the surface area of the fuel rods

Now we need to calculate the surface area of the fuel rods that are in contact with the soil for the heat transfer. The calculation is as follows: Surface Area = π × D × L Surface Area = π × 0.0833 ft × 3 ft Surface Area ≈ 0.78 ft²
04

Calculate the rate of heat transfer

Now we can calculate the rate of heat transfer from the fuel rods to the atmosphere through the soil. We will use the following formula: q = k × (Surface Area) × (ΔT / Distance) q = 0.6 Btu/h·ft·F × 0.78 ft² × (290°F / 15 ft) q ≈ 9.42 Btu/h Thus, the rate of heat transfer from the fuel rods to the atmosphere through the soil is approximately 9.42 Btu/h.

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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 fundamental property that measures a material's ability to conduct heat. It's often denoted by the symbol \( k \) and is generally expressed in units of \( \text{Btu/h}\cdot\text{ft}\cdot{}^\circ\text{F} \). This property tells us how much heat will be transferred through a material per unit time for a given temperature difference per unit thickness.
For example, in our fuel rods exercise, the thermal conductivity of the soil is given as \( 0.6 \text{ Btu/h} \cdot \text{ft} \cdot {}^\circ F \). This indicates that for every one degree Fahrenheit temperature difference across one foot of soil, 0.6 Btu of heat energy is transferred in one hour.
Understanding thermal conductivity is essential when dealing with heat transfer in materials because it influences how fast or slow heat moves through a substance. A higher thermal conductivity means that the material is better at conducting heat, which is important in applications where heat dissipation is crucial.
Temperature Difference
The temperature difference, often represented by \( \Delta T \), is a principal factor in determining the rate of heat transfer between two substances or locations. It's simply the difference in temperature between one point and another, driving the flow of heat. In our exercise, the temperature difference is between the surface of the uranium fuel rods and the surface of the ground, which are \( 350^{\circ} \text{F} \) and \( 60^{\circ} \text{F} \) respectively.
The way we calculate this difference is straightforward: \( \Delta T = T_1 - T_2 \), where \( T_1 \) is the higher temperature and \( T_2 \) is the lower temperature. For our scenario, \( \Delta T = 350^{\circ} \text{F} - 60^{\circ} \text{F} = 290^{\circ} \text{F} \).
Temperature difference plays a critical role in heat transfer because it's the driving force behind the movement of heat. The larger the temperature difference, the greater the potential for heat flow, which is why calculating it accurately is so vital in any thermal analysis.
Surface Area Calculation
Calculation of surface area is a key component in determining how much heat will be transferred between a solid object and its surrounding environment. In many heat transfer situations, the surface area through which the heat is being transferred can greatly affect the rate of heat flow.
For the fuel rods, the relevant surface area is the lateral surface area in contact with the surrounding soil. Assuming the rods are cylindrical, this area is calculated using the formula for the lateral surface area: \( \text{Surface Area} = \pi \times D \times L \), where \( D \) is the diameter, and \( L \) is the length of the cylinder.
In this exercise, \( D = 0.0833 \) ft (converted from 1 inch), and \( L = 3 \) ft. Plugging these values into the formula gives \( \text{Surface Area} = \pi \times 0.0833 \times 3 \approx 0.78 \text{ ft}^2 \).
Accurate surface area calculation ensures that we correctly estimate how much heat is being transferred. The greater the surface area, the higher the rate of heat exchange, assuming all other factors are constant.
Rate of Heat Transfer
The rate of heat transfer indicates how quickly heat energy moves from one place or object to another. It's a crucial metric in thermal management and is influenced by several factors, including thermal conductivity, temperature difference, and surface area.
To calculate the rate of heat transfer, the following formula is utilized:
  • \( q = k \times \text{(Surface Area)} \times \left(\frac{\Delta T}{\text{Distance}}\right) \)
Where:
  • \( q \) represents the rate of heat transfer in Btu/h,
  • \( k \) is the thermal conductivity of the material,
  • \( \Delta T \) is the temperature difference,
  • Distance refers to the path through which the heat operates.
Substituting our values gives \( q = 0.6 \times 0.78 \times \frac{290}{15} \approx 9.42 \text{ Btu/h} \).
This result means that approximately 9.42 Btu of heat is being transferred every hour from each rod to the surroundings through the soil. Understanding this rate helps engineers design systems that can adequately manage heat transfer, whether they need to minimize heat loss or enhance cooling efficiency.

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Most popular questions from this chapter

What is the reason for the widespread use of fins on surfaces?

We are interested in steady state heat transfer analysis from a human forearm subjected to certain environmental conditions. For this purpose consider the forearm to be made up of muscle with thickness \(r_{m}\) with a skin/fat layer of thickness \(t_{s f}\) over it, as shown in the Figure P3-138. For simplicity approximate the forearm as a one-dimensional cylinder and ignore the presence of bones. The metabolic heat generation rate \(\left(\dot{e}_{m}\right)\) and perfusion rate \((\dot{p})\) are both constant throughout the muscle. The blood density and specific heat are \(\rho_{b}\) and \(c_{b}\), respectively. The core body temperate \(\left(T_{c}\right)\) and the arterial blood temperature \(\left(T_{a}\right)\) are both assumed to be the same and constant. The muscle and the skin/fat layer thermal conductivities are \(k_{m}\) and \(k_{s f}\), respectively. The skin has an emissivity of \(\varepsilon\) and the forearm is subjected to an air environment with a temperature of \(T_{\infty}\), a convection heat transfer coefficient of \(h_{\text {conv }}\), and a radiation heat transfer coefficient of \(h_{\mathrm{rad}}\). Assuming blood properties and thermal conductivities are all constant, \((a)\) write the bioheat transfer equation in radial coordinates. The boundary conditions for the forearm are specified constant temperature at the outer surface of the muscle \(\left(T_{i}\right)\) and temperature symmetry at the centerline of the forearm. \((b)\) Solve the differential equation and apply the boundary conditions to develop an expression for the temperature distribution in the forearm. (c) Determine the temperature at the outer surface of the muscle \(\left(T_{i}\right)\) and the maximum temperature in the forearm \(\left(T_{\max }\right)\) for the following conditions: $$ \begin{aligned} &r_{m}=0.05 \mathrm{~m}, t_{s f}=0.003 \mathrm{~m}, \dot{e}_{m}=700 \mathrm{~W} / \mathrm{m}^{3}, \dot{p}=0.00051 / \mathrm{s} \\ &T_{a}=37^{\circ} \mathrm{C}, T_{\text {co }}=T_{\text {surr }}=24^{\circ} \mathrm{C}, \varepsilon=0.95 \\ &\rho_{b}=1000 \mathrm{~kg} / \mathrm{m}^{3}, c_{b}=3600 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k_{m}=0.5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K} \\ &k_{s f}=0.3 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, h_{\text {conv }}=2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}, h_{\mathrm{rad}}=5.9 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K} \end{aligned} $$

Explain how the fins enhance heat transfer from a surface. Also, explain how the addition of fins may actually decrease heat transfer from a surface.

Consider a wall that consists of two layers, \(A\) and \(B\), with the following values: \(k_{A}=0.8 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, L_{A}=8 \mathrm{~cm}, k_{B}=\) \(0.2 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, L_{B}=5 \mathrm{~cm}\). If the temperature drop across the wall is \(18^{\circ} \mathrm{C}\), the rate of heat transfer through the wall per unit area of the wall is (a) \(180 \mathrm{~W} / \mathrm{m}^{2}\) (b) \(153 \mathrm{~W} / \mathrm{m}^{2}\) (c) \(89.6 \mathrm{~W} / \mathrm{m}^{2}\) (d) \(72 \mathrm{~W} / \mathrm{m}^{2}\) (e) \(51.4 \mathrm{~W} / \mathrm{m}^{2}\)

Steam in a heating system flows through tubes whose outer diameter is \(5 \mathrm{~cm}\) and whose walls are maintained at a temperature of \(180^{\circ} \mathrm{C}\). Circular aluminum alloy 2024-T6 fins \((k=186 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) of outer diameter \(6 \mathrm{~cm}\) and constant thickness \(1 \mathrm{~mm}\) are attached to the tube. The space between the fins is \(3 \mathrm{~mm}\), and thus there are 250 fins per meter length of the tube. Heat is transferred to the surrounding air at \(T_{\infty}=25^{\circ} \mathrm{C}\), with a heat transfer coefficient of \(40 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the increase in heat transfer from the tube per meter of its length as a result of adding fins.

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