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A hot surface at \(80^{\circ} \mathrm{C}\) in air at \(20^{\circ} \mathrm{C}\) is to be cooled by attaching 10 -cm-long and 1 -cm-diameter cylindrical fins. The combined heat transfer coefficient is \(30 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and heat transfer from the fin tip is negligible. If the fin efficiency is \(0.75\), the rate of heat loss from 100 fins is (a) \(325 \mathrm{~W}\) (b) \(707 \mathrm{~W}\) (c) \(566 \mathrm{~W}\) (d) \(424 \mathrm{~W}\) (e) \(754 \mathrm{~W}\)

Short Answer

Expert verified
In this problem, we are given the parameters of cylindrical fins attached to a hot surface and asked to find the rate of heat loss from 100 fins. We calculated the area of one fin, the temperature difference, the heat transfer rate of one fin, and finally the total heat transfer rate. The total heat transfer rate for 100 fins is approximately 424.3 W.

Step by step solution

01

Calculate the fin area

To calculate the heat transfer, we need to find the area of one fin. The fin is cylindrical with a length of 10 cm and a diameter of 1 cm. The surface area of a cylinder (excluding the top and bottom) can be found using the following formula: \(A_\text{fin} = 2 \pi r_\text{fin} L_\text{fin}\) where: \(A_\text{fin}\): the surface area of one fin \(r_\text{fin}= \dfrac{D_\text{fin}}{2}\): the radius of the fin \(L_\text{fin}\): the length of the fin We convert the length and diameter to meters and substitute the given values into the formula: \(r_\text{fin} = \dfrac{0.01 \, \text{m}}{2} = 0.005 \, \text{m}\) \(L_\text{fin} = 0.1 \, \text{m}\) \(A_\text{fin} = 2 \pi (0.005 \, \text{m}) (0.1 \, \text{m}) = 0.00314 \, \text{m}^2\)
02

Calculate the temperature difference

Next, we need to find the temperature difference between the hot surface and the air. This is given by: \(\Delta T = T_\text{surface} - T_\text{air}\) Substituting the given values: \(\Delta T = 80^{\circ} \mathrm{C} - 20^{\circ} \mathrm{C} = 60 \mathrm{~K}\)
03

Calculate the heat transfer rate of one fin

Now we can find the heat transfer rate of one fin using the formula: \(q_\text{fin} = h A_\text{fin} \eta_\text{fin} \Delta T\) where: \(q_\text{fin}\): the heat transfer rate of one fin \(h\): the combined heat transfer coefficient \(\eta_\text{fin}\): the fin efficiency \(\Delta T\): the temperature difference Substituting the given values and the values calculated in the previous steps: \(q_\text{fin} = (30 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}) (0.00314 \, \text{m}^2) (0.75) (60 \mathrm{~K}) = 4.243 \mathrm{~W}\)
04

Calculate the total heat transfer rate

Lastly, we multiply the heat transfer rate of one fin by the total number of fins to obtain the total heat transfer rate: \(q_\text{total} = N_\text{fins} q_\text{fin}\) Substituting the given number of fins and the value calculated in the previous step: \(q_\text{total} = 100 \; (4.243 \mathrm{~W}) = 424.3 \mathrm{~W}\) Now we can see that the answer is closest to option (d) \(424 \mathrm{~W}\).

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Key Concepts

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

Fin Efficiency
The efficiency of a fin, also known as the fin efficiency (\( \eta_{\text{fin}}\)), describes how effectively a fin transfers heat relative to its potential. It's calculated as the ratio of the actual heat transfer to the maximum possible heat transfer, assuming the entire fin is at the base temperature. This provides a measure of performance, indicating how much of the fin's potential is realized in practice. For example, in our scenario the fin efficiency is given as 0.75, meaning 75% of the ideal heat removal is achieved. This efficiency can be impacted by several factors:
  • Material conductivity: Higher thermal conductivity materials will typically yield higher fin efficiencies.
  • Fin geometry: The shape and size influence the ability to dissipate heat effectively.
  • Operating environment: The surrounding fluid medium can affect heat transfer coefficients.
Understanding fin efficiency helps engineers optimize design for better performance.
Cylindrical Fins
Cylindrical fins, as the name suggests, are fins shaped like cylinders. They are commonly used in heat dissipation applications, such as cooling electronic devices and engine components. In this problem, the fin is described as being 10 cm long with a 1 cm diameter. This geometry helps increase the surface area for heat exchange without consuming much space. The key components we consider when analyzing cylindrical fins include:
  • Length and diameter: These influence the surface area for heat transfer.
  • Surface area calculation: As shown, the surface area is critical for determining overall heat loss.
  • Material choice: Determines how fast heat can be conducted across the fin.
The simplicity of manufacturing and the efficiency of heat transfer make cylindrical fins a popular choice in many cooling applications.
Combined Heat Transfer Coefficient
The combined heat transfer coefficient (\( h \)) represents the ability of the surface to transfer heat, combining effects due to conduction, convection, and radiation. It is crucial for calculating the rate of heat loss in systems involving fins. It is expressed in units of \( \text{W/m}^2 \cdot \text{K} \). In this problem, the coefficient is provided as 30 \( \text{W/m}^2 \cdot \text{K} \). This value allows us to calculate the thermal performance of the fins through the following factors:
  • Material properties: Different materials conduct heat in distinct ways.
  • Surface conditions: Smooth versus rough surfaces affect how air flows over the fins.
  • Flow conditions: The rate and nature of airflow impact convective heat transfer.
This coefficient is vital for determining the overall effectiveness of heat dissipation in the designed system.
Temperature Difference
Temperature difference, denoted as \( \Delta T \), is the driving force behind heat transfer. It is the difference between the temperature of a surface and the surrounding medium. Here, the hot surface temperature is \( 80^{\circ} C \), and the air temperature is \( 20^{\circ} C \), resulting in a \( \Delta T \) of \( 60 \mathrm{~K} \). This difference directly influences the rate of heat transfer:
  • Greater temperature difference: Leads to higher heat transfer rate.
  • Stability: Constant temperature differences suggest consistent heat transfer rates.
  • Temperature gradients: They determine the direction and efficiency of heat flow.
For engineers, it is important because it helps predict how quickly a system can reach thermal equilibrium, which is vital for preventing overheating or maintaining desired operating temperatures.

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Most popular questions from this chapter

A pipe is insulated such that the outer radius of the insulation is less than the critical radius. Now the insulation is taken off. Will the rate of heat transfer from the pipe increase or decrease for the same pipe surface temperature?

Consider a stainless steel spoon \(\left(k=8.7 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\right)\) partially immersed in boiling water at \(200^{\circ} \mathrm{F}\) in a kitchen at \(75^{\circ} \mathrm{F}\). The handle of the spoon has a cross section of \(0.08\) in \(\times\) \(0.5\) in, and extends 7 in in the air from the free surface of the water. If the heat transfer coefficient at the exposed surfaces of the spoon handle is \(3 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\), determine the temperature difference across the exposed surface of the spoon handle. State your assumptions. Answer: \(124.6^{\circ} \mathrm{F}\)

Hot water at an average temperature of \(70^{\circ} \mathrm{C}\) is flowing through a \(15-\mathrm{m}\) section of a cast iron pipe \((k=52 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) whose inner and outer diameters are \(4 \mathrm{~cm}\) and \(4.6 \mathrm{~cm}\), respectively. The outer surface of the pipe, whose emissivity is \(0.7\), is exposed to the cold air at \(10^{\circ} \mathrm{C}\) in the basement, with a heat transfer coefficient of \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The heat transfer coefficient at the inner surface of the pipe is \(120 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Taking the walls of the basement to be at \(10^{\circ} \mathrm{C}\) also, determine the rate of heat loss from the hot water. Also, determine the average velocity of the water in the pipe if the temperature of the water drops by \(3^{\circ} \mathrm{C}\) as it passes through the basement.

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: $$ \begin{aligned} &r_{m}=0.05 \mathrm{~m}, t_{s f}=0.003 \mathrm{~m}, \dot{e}_{m}=700 \mathrm{~W} / \mathrm{m}^{3}, \dot{p}=0.00051 / \mathrm{s} \\ &T_{a}=37^{\circ} \mathrm{C}, T_{\text {co }}=T_{\text {surr }}=24^{\circ} \mathrm{C}, \varepsilon=0.95 \\ &\rho_{b}=1000 \mathrm{~kg} / \mathrm{m}^{3}, c_{b}=3600 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k_{m}=0.5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K} \\ &k_{s f}=0.3 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, h_{\text {conv }}=2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}, h_{\mathrm{rad}}=5.9 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K} \end{aligned} $$

A 3-cm-long, 2-mm \(\times 2-\mathrm{mm}\) rectangular crosssection aluminum fin \((k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) is attached to a surface. If the fin efficiency is 65 percent, the effectiveness of this single fin is (a) 39 (b) 30 (c) 24 (d) \(18 \quad(e) 7\)

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