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Circular fins of uniform cross section, with diameter of \(10 \mathrm{~mm}\) and length of \(50 \mathrm{~mm}\), are attached to a wall with surface temperature of \(350^{\circ} \mathrm{C}\). The fins are made of material with thermal conductivity of \(240 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), they are exposed to an ambient air condition of \(25^{\circ} \mathrm{C}\), and the convection heat transfer coefficient is $250 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Determine the heat transfer rate and plot the temperature variation of a single fin for the following boundary conditions: (a) Infinitely long fin (b) Adiabatic fin tip (c) Fin with tip temperature of \(250^{\circ} \mathrm{C}\) (d) Convection from the fin tip

Short Answer

Expert verified
Question: Calculate the heat transfer rate and plot the temperature variation for a fin with the given dimensions and material properties for four different boundary conditions: (a) infinitely long fin, (b) adiabatic fin tip, (c) fin with tip temperature of 250°C, and (d) convection from the fin tip. Diameter of the fin, D = 10 mm; Length of the fin, L = 50 mm; Surface temperature of the wall, T_s = 350 °C; Ambient temperature, T_inf = 25 °C; Thermal conductivity, k = 240 W/(m.K); Convective heat transfer coefficient, h = 250 W/(m².K).

Step by step solution

01

General Information and Constants

Diameter of the fin, D = 10 mm = 0.01 m Length of the fin, L = 50 mm = 0.05 m Surface temperature of the wall, T_s = 350 °C Ambient temperature, T_inf = 25 °C Thermal conductivity, k = 240 W/(m.K) Convective heat transfer coefficient, h = 250 W/(m².K) Fin area, A_fin = pi * D * L = 0.01 * pi * 0.05 m² Perimeter of fin, P = pi * D = 0.01 * pi m Now let's analyze the heat transfer for each boundary condition.
02

(a) Infinitely Long Fin

An infinitely long fin implies that heat is only lost through convection on the surface and not at the fin tip. So, for the infinitely long fin, we have to find the temperature distribution and the heat transfer rate. 1. Calculate the fin parameter, m: \(m = \sqrt{\frac{h \cdot P}{k \cdot A_c}}\) where \(A_c\) is the cross-sectional area of the fin. \(A_c = \frac{\pi \cdot D^2}{4} = \frac{\pi \cdot (0.01)^2}{4} \mathrm{m}^2\) 2. Find the temperature distribution for an infinitely long fin, T(x): \(T(x) = T_s - (T_s - T_{\infty})(e^{-mx})\) 3. Plot T(x) vs x for the fin. 4. Determine the heat transfer rate for a single fin, q_fin: \(q_{\text{fin}} = h \cdot A_{\text{fin}} \cdot \Big( \frac{T_s - T_{\infty}}{\frac{k \cdot A_c}{m} + \frac{1}{h \cdot P}} \Big)\)
03

(b) Adiabatic Fin Tip

An adiabatic fin tip means that there is no heat loss at the fin tip (x = L). The fin equation remains the same, but we change the boundary condition for the fin tip temperature. Here, the boundary condition at x = L is that dT/dx = 0. 1. Solve the fin equation with the new boundary condition to find the temperature distribution, T(x). 2. Plot T(x) vs x for the fin. 3. Find the heat transfer rate for a single fin, q_fin, using the same equation as in (a).
04

(c) Fin with Tip Temperature of 250°C

For this case, the boundary condition at x = L is T(L) = 250°C. 1. Solve the fin equation with the new boundary condition to find the temperature distribution, T(x). 2. Plot T(x) vs x for the fin. 3. Find the heat transfer rate for a single fin, q_fin, using the same equation as in (a).
05

(d) Convection from the Fin Tip

In this case, heat is being lost through convection even at the fin tip. 1. Set up a new fin equation accounting for the convection from the fin tip. 2. Solve the fin equation to find the temperature distribution, T(x). 3. Plot T(x) vs x for the fin. 4. Find the heat transfer rate for a single fin, q_fin, using the same equation as in (a). By following these steps for each of the four boundary conditions, the heat transfer rate and the temperature distribution for each case can be found and plotted.

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Most popular questions from this chapter

Consider a wall that consists of two layers, \(A\) and \(B\), with the following values: $k_{A}=1.2 \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) \(56.8 \mathrm{~W} / \mathrm{m}^{2}\) (b) \(72.1 \mathrm{~W} / \mathrm{m}^{2}\) (c) \(114 \mathrm{~W} / \mathrm{m}^{2}\) (d) \(201 \mathrm{~W} / \mathrm{m}^{2}\) (e) \(270 \mathrm{~W} / \mathrm{m}^{2}\)

A mixture of chemicals is flowing in a pipe $\left(k=14 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, D_{i}=2.5 \mathrm{~cm}, D_{\rho}=3 \mathrm{~cm}\right.\(, and \)L=10 \mathrm{~m}$ ). During the transport, the mixture undergoes an exothermic reaction having an average temperature of \(135^{\circ} \mathrm{C}\) and a convection heat transfer coefficient of $150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. To prevent any incident of thermal burn, the pipe needs to be insulated. However, due to the vicinity of the pipe, there is only enough room to fit a \(2.5\)-cm-thick layer of insulation over the pipe. The pipe is situated in a plant where the average ambient air temperature is \(20^{\circ} \mathrm{C}\) and the convection heat transfer coefficient is \(25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the insulation for the pipe such that the thermal conductivity of the insulation is sufficient to maintain the outside surface temperature at \(45^{\circ} \mathrm{C}\) or lower.

Consider a flat ceiling that is built around $38-\mathrm{mm} \times 90-\mathrm{mm}\( wood studs with a center-to-center distance of \)400 \mathrm{~mm}\(. The lower part of the ceiling is finished with \)13-\mathrm{mm}$ gypsum wallboard, while the upper part consists of a wood subfloor \(\left(R=0.166 \mathrm{~m}^{2},{ }^{\circ} \mathrm{C} / \mathrm{W}\right)\), a 13 -mm plywood layer, a layer of felt $\left(R=0.011 \mathrm{~m}^{2},{ }^{\circ} \mathrm{C} / \mathrm{W}\right)\(, and linoleum \)\left(R=0.009 \mathrm{~m}^{2},{ }^{\circ} \mathrm{C} / \mathrm{W}\right)$. Both sides of the ceiling are exposed to still air. The airspace constitutes 82 percent of the heat transmission area, while the studs and headers constitute 18 percent. Determine the winter \(R\)-value and the \(U\)-factor of the ceiling assuming the 90 -mm-wide airspace between the studs \((a)\) does not have any reflective surface, \((b)\) has a reflective surface with \(\varepsilon=0.05\) on one side, and \((c)\) has reflective surfaces with \(\varepsilon=0.05\) on both sides. Assume a mean temperature of \(10^{\circ} \mathrm{C}\) and a temperature difference of \(5.6^{\circ} \mathrm{C}\) for the airspace.

The \(700 \mathrm{~m}^{2}\) ceiling of a building has a thermal resistance of \(0.52 \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\). The rate at which heat is lost through this ceiling on a cold winter day when the ambient temperature is \(-10^{\circ} \mathrm{C}\) and the interior is at \(20^{\circ} \mathrm{C}\) is (a) \(23.1 \mathrm{~kW}\) (b) \(40.4 \mathrm{~kW}\) (c) \(55.6 \mathrm{~kW}\) (d) \(68.1 \mathrm{~kW}\) (e) \(88.6 \mathrm{~kW}\)

A spherical vessel, \(3.0 \mathrm{~m}\) in diameter (and negligible wall thickness), is used for storing a fluid at a temperature of $0^{\circ} \mathrm{C}\(. The vessel is covered with a \)5.0$-cm-thick layer of an insulation \((k=0.20 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). The surrounding air is at \(22^{\circ} \mathrm{C}\). The inside and outside heat transfer coefficients are 40 and 10 $\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\(, respectively. Calculate \)(a)$ all thermal resistances, in \(\mathrm{K} / \mathrm{W},(b)\) the steady rate of heat transfer, and \((c)\) the temperature difference across the insulation layer.

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