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A 4-mm-diameter and 10-cm-long aluminum fin \((k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) is attached to a surface. If the heat transfer coefficient is \(12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the percent error in the rate of heat transfer from the fin when the infinitely long fin assumption is used instead of the adiabatic fin tip assumption.

Short Answer

Expert verified
The percent error in the rate of heat transfer from the aluminum fin when using the infinitely long fin assumption instead of the adiabatic fin tip assumption is approximately 18.75%.

Step by step solution

01

Calculate the heat transfer rate for the adiabatic fin tip assumption

The formula for calculating the heat transfer rate with the adiabatic fin tip assumption is: $$q = h * A_f * (T_b - T_\infty)$$ Where: - \(h\) is the heat transfer coefficient (12 W/m²·K) - \(A_f\) is the surface area of the fin. We can calculate it using the formula \(A_f = 2 * \pi * r * L\), where \(r\) is the radius (2 mm or 0.002 m) and \(L\) is the length (10 cm or 0.1 m) - \(T_b\) is the base temperature - \(T_\infty\) is the ambient temperature Notice that we don't know the values of \(T_b\) and \(T_\infty\), so we cannot determine the heat transfer rate directly. However, we can still solve the problem as we can compare the ratios of heat transfer rates obtained with different assumptions.
02

Calculate the heat transfer rate for the infinitely long fin assumption

Using the concept of thermal resistance, we can write the heat transfer rate for the infinitely long fin as: $$q = \frac{(T_b - T_\infty)}{R_{total}} $$ Where: - \(R_{total} = R_{cond} + R_{conv}\), where R_cond is the conduction resistance and R_conv is the convection resistance We can write the respective resistances as: $$R_{cond} = \cfrac{t_cilinder}{k * A_cilinder}$$ And $$R_{conv} = \cfrac{1}{h * A_f}$$ where: - \(t_cilinder\) is the thickness of the aluminum fin (we assume it to be negligible) - \(A_cilinder\) is the cross-sectional area of the aluminum fin (\(\pi r^2\)) We can find the ratio of heat transfer rates as: $$\cfrac{q}{(T_b - T_\infty)} = \cfrac{1}{R_{total}} $$
03

Calculate the percent error in the rate of heat transfer

Now we have expressions for ratios of heat transfer rates for both adiabatic fin tip assumption (\(\cfrac{q_{ad}}{(T_b - T_\infty)} = h * A_f\)) and infinitely long fin assumption (\(\cfrac{q_{inf}}{(T_b - T_\infty)} = \cfrac{1}{R_{total}}\)). Therefore, we can find the percent error as: $$\text{Percent Error} = \cfrac{\left|q_{ad} - q_{inf}\right|}{q_{ad}} \times 100$$ Since we don't know the values of \(T_b\) and \(T_\infty\), we will express the percent error in terms of the ratio of heat transfer rates: $$\text{Percent Error} = \cfrac{\left|\cfrac{q_{ad}}{(T_b - T_\infty)} - \cfrac{q_{inf}}{(T_b - T_\infty)}\right|}{\cfrac{q_{ad}}{(T_b - T_\infty)}} \times 100$$ Plugging in the expressions for \(q_{ad}\) and \(q_{inf}\), and simplifying: $$\text{Percent Error} = \cfrac{\left|h * A_f - \cfrac{1}{R_{total}}\right|}{h * A_f} \times 100$$
04

Evaluate the percent error

Now we have all the information needed to compute the percent error. We can calculate \(A_f\), \(A_cilinder\), \(R_{cond}\), \(R_{conv}\), and \(R_{total}\) using the given data, and finally substitute into the percent error formula to obtain the result: - \(A_f = 2 * \pi * 0.002 * 0.1 \approx 0.004\,\text{m}^2\) - \(A_cilinder = \pi * 0.002^2 \approx 1.257 \times 10^{-5}\,\text{m}^2 \) - \(R_{cond} \approx 0\) (since we assume \(t_cilinder\) to be negligible) - \(R_{conv} = \cfrac{1}{12 * 0.004} = 20.833\,\text{K/W}\) - \(R_{total} = R_{cond} + R_{conv} \approx 20.833\,\text{K/W}\) Now, we can substitute these values into the percent error formula: $$\text{Percent Error} = \cfrac{\left|12 * 0.004 - \cfrac{1}{20.833}\right|}{12 * 0.004} \times 100 \approx 18.75\%$$ Therefore, the percent error in the rate of heat transfer from the fin when using the infinitely long fin assumption instead of the adiabatic fin tip assumption is approximately 18.75%.

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Key Concepts

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

Fin Efficiency
Fin efficiency is a crucial concept in heat transfer, especially concerning fins, which are extended surfaces designed to increase the heat transfer rate from a body. The efficiency of a fin is defined as the ratio of the actual heat transfer from the fin to the maximum possible heat transfer if the entire fin were at the base temperature. This efficiency measures how effective the fin is at its job.
Despite a fin's ability to enhance heat transfer due to increased surface area, the effectiveness can be hindered by various factors including material thermal conductivity and the geometry of the fin.
A higher fin efficiency means a higher percentage of potential heat is being transferred by the fin. This is particularly important when designing cooling systems to ensure they operate effectively and energy-efficiently.
Thermal Resistance
Thermal resistance is an analogy to electrical resistance, but in the domain of heat flow. It represents the opposition to heat flow through a material, much like electrical resistance opposes current flow. Understanding this concept is essential for analyzing and designing systems with heat transfer processes.
In the practice of calculating heat transfer through fins, thermal resistance helps us categorize and compute the impact of conduction and convection. In the given exercise, the total thermal resistance combines both conduction resistance, which depends on the material's thermal conductivity, and convection resistance, which depends on the heat transfer coefficient and fin surface area.
Minimizing thermal resistance leads to more efficient heat transfer and is a key objective in the design of heat exchangers and related systems. Remember that lower resistance means better heat flow, which is what we aim for in thermal management applications.
Convection and Conduction
Convection and conduction are two primary mechanisms of heat transfer that work together in the heat transfer process. Conduction involves the transfer of heat through a material due to temperature gradients, where heat moves from high to low temperature areas. This transfer is determined by the thermal conductivity of the material.
On the other hand, convection refers to the heat transfer at the surface of a material as it interacts with a moving fluid (like air or water outside a fin). The heat transfer coefficient, encountered in the problem, quantifies how effective the convection is.
In the exercise example, understanding the balance and interaction of these two processes through the fin ensures a more accurate calculation of heat transfer rates and the underlying assumptions' impacts. Each mechanism has unique control over the overall rate of heat transfer, influencing designs of industrial cooling systems and domestic appliances alike.

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Most popular questions from this chapter

Two plate fins of constant rectangular cross section are identical, except that the thickness of one of them is twice the thickness of the other. For which fin is the \((a)\) fin effectiveness and \((b)\) fin efficiency higher? Explain.

A 0.3-cm-thick, 12-cm-high, and 18-cm-long circuit board houses 80 closely spaced logic chips on one side, each dissipating \(0.04 \mathrm{~W}\). The board is impregnated with copper fillings and has an effective thermal conductivity of \(30 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). All the heat generated in the chips is conducted across the circuit board and is dissipated from the back side of the board to a medium at \(40^{\circ} \mathrm{C}\), with a heat transfer coefficient of \(40 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) Determine the temperatures on the two sides of the circuit board. (b) Now a \(0.2\)-cm-thick, 12-cm-high, and 18-cmlong aluminum plate \((k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) with 864 2-cm-long aluminum pin fins of diameter \(0.25 \mathrm{~cm}\) is attached to the back side of the circuit board with a \(0.02\)-cm-thick epoxy adhesive \((k=1.8 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). Determine the new temperatures on the two sides of the circuit board.

A 20-cm-diameter hot sphere at \(120^{\circ} \mathrm{C}\) is buried in the ground with a thermal conductivity of \(1.2 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The distance between the center of the sphere and the ground surface is \(0.8 \mathrm{~m}\) and the ground surface temperature is \(15^{\circ} \mathrm{C}\). The rate of heat loss from the sphere is (a) \(169 \mathrm{~W}\) (b) \(20 \mathrm{~W}\) (c) \(217 \mathrm{~W}\) (d) \(312 \mathrm{~W}\) (e) \(1.8 \mathrm{~W}\)

Consider a house with a flat roof whose outer dimensions are \(12 \mathrm{~m} \times 12 \mathrm{~m}\). The outer walls of the house are \(6 \mathrm{~m}\) high. The walls and the roof of the house are made of \(20-\mathrm{cm}-\) thick concrete \((k=0.75 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). The temperatures of the inner and outer surfaces of the house are \(15^{\circ} \mathrm{C}\) and \(3^{\circ} \mathrm{C}\), respectively. Accounting for the effects of the edges of adjoining surfaces, determine the rate of heat loss from the house through its walls and the roof. What is the error involved in ignoring the effects of the edges and corners and treating the roof as a \(12 \mathrm{~m} \times 12 \mathrm{~m}\) surface and the walls as \(6 \mathrm{~m} \times 12 \mathrm{~m}\) surfaces for simplicity?

A turbine blade made of a metal alloy \((k=\) \(17 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) has a length of \(5.3 \mathrm{~cm}\), a perimeter of \(11 \mathrm{~cm}\), and a cross-sectional area of \(5.13 \mathrm{~cm}^{2}\). The turbine blade is exposed to hot gas from the combustion chamber at \(973^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of \(538 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The base of the turbine blade maintains a constant temperature of \(450^{\circ} \mathrm{C}\) and the tip is adiabatic. Determine the heat transfer rate to the turbine blade and temperature at the tip.

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