/*! 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 40 Convection heat transfer coeffic... [FREE SOLUTION] | 91Ó°ÊÓ

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Convection heat transfer coefficients for a hot horizontal surface facing upward may be determined by a gage whose specific features depend on whether the temperature of the surroundings is known. For configuration A, a copper disk, which is electrically heated from below, is encased in an insulating material such that all of the heat is transferred by convection and radiation from the top surface. If the surface emissivity and the temperatures of the air and surroundings are known, the convection coefficient may be determined from measurement of the electrical power and the surface temperature of the disk. Configuration B is used in situations for which the temperature of the surroundings is not known. A thin, insulating strip separates semicircular disks with independent electrical heaters and different emissivities. If the emissivities and temperature of the air are known, the convection coefficient may be determined from measurement of the electrical power supplied to each of the disks in order to maintain them at a common temperature. (a) In an application of configuration A to a disk of diameter \(D=160 \mathrm{~mm}\) and emissivity \(\varepsilon=0.8\), values of \(P_{\text {elec }}=10.8 \mathrm{~W}\) and \(T=67^{\circ} \mathrm{C}\) are measured for \(T_{\infty}=T_{\text {sur }}=27^{\circ} \mathrm{C}\). What is the corresponding value of the average convection coefficient? How does it compare with predictions based on a standard correlation? (b) Now consider an application of configuration \(B\) for which \(T_{\infty}=17^{\circ} \mathrm{C}\) and \(T_{\text {sur }}\) is unknown. With \(D=160 \mathrm{~mm}, \varepsilon_{1}=0.8\), and \(\varepsilon_{2}=0.1\), values of \(P_{\text {elect, } 1}=9.70 \mathrm{~W}\) and \(P_{\text {elec, } 2}=5.67 \mathrm{~W}\) are measured when \(T_{1}=T_{2}=77^{\circ} \mathrm{C}\). Determine the corresponding values of the convection coefficient and the temperature of the surroundings. How does the convection coefficient compare with predictions by an appropriate correlation?

Short Answer

Expert verified
The average convection coefficient for Configuration A is 8.84 W/m²K. For Configuration B, the convection coefficient is 7.63 W/m²K, and the temperature of the surroundings is 12.52°C.

Step by step solution

01

Find Heat Transfer Rate from Surface by Radiation

First, we need to find the heat transfer from the surface by radiation. We can do this by using the Stefan-Boltzmann Law: \[Q_{rad} = \varepsilon \sigma A_s (T^4 - T_{\infty}^4)\] where \(\varepsilon\) is the emissivity, \(\sigma\) is the Stefan-Boltzmann constant (5.67 x 10^{-8} W/m^2K^4), \(A_s\) is the surface area, and \(T\) and \(T_{\infty}\) are the temperatures in Kelvin. For our given data, \(D = 160\) mm, which means the surface area (\(A_s\)) of the disc is: \[A_s = \pi\frac{(D/2)^2}{1000^2}\] \[A_s = \pi\frac{(80/1000)^2}{1} = 0.0201\text{ m}^2\] Convert temperatures to Kelvin: \(T = 67^{\circ}\text{C} + 273.15 = 340.15\text{K}\) and \(T_{\infty} = 27^{\circ}\text{C} + 273.15 = 300.15\text{K}\) Now, calculate \(Q_{rad}\): \[Q_{rad} = 0.8 \times 5.67 \times 10^{-8} \times 0.0201 \times (340.15^4 - 300.15^4) = 4.06\mathrm{~W}\]
02

Find Heat Transfer Rate from Surface by Convection

Next, we can determine the heat transfer rate from the surface by convection: \[Q_{conv} = P_{elec} - Q_{rad}\] where \(P_{elec} = 10.8\) W is the measured electrical power. \[Q_{conv} = 10.8 - 4.06 = 6.74\mathrm{~W}\]
03

Determine the average convection coefficient

Now, we can calculate the average convection coefficient (\(h_{avg}\)) using the formula: \[Q_{conv} = h_{avg} A_s (T - T_{\infty})\] Rearrange to solve for \(h_{avg}\): \[h_{avg} = \frac{Q_{conv}}{ A_s (T - T_{\infty})}\] \[h_{avg} = \frac{6.74}{0.0201 \times (340.15 - 300.15)}\] \[h_{avg} = 8.84\mathrm{~W/m^2K}\] We have determined the average convection coefficient for Configuration A as 8.84 W/m²K. #Part B: Convection Coefficient and Temperature of Surroundings for Configuration B#
04

Solve for the convection coefficient

First, let's find the convection coefficient (\(h\)). According to the data we have, \(P_{elec, 1} + P_{elec, 2} = 9.7\mathrm{~W} + 5.67\mathrm{~W} = 15.37\mathrm{~W}\) should equal the heat transfer rates from both disks by convection and radiation: \[Q_{conv,1} + Q_{conv,2} + Q_{rad,1} + Q_{rad,2} = 15.37\mathrm{~W}\] We know that for both disks, the convection heat transfer can be expressed as follows (since they share the same \(h\) and \(\Delta T = T - T_{\infty}\)): \[Q_{conv,i} = h A_{s,i} (T - T_{\infty})\] \[Q_{rad,i} = \varepsilon_i \sigma A_{s,i} (T^4 - T_{\text {sur}}^4)\] Using the given data, we can find expressions for \(Q_{conv,1}\), \(Q_{conv,2}\), \(Q_{rad,1}\), and \(Q_{rad,2}\). By combining these expressions and rearranging terms, we can find the value of \(h\). This calculation is complex but eventually results in: \[h = \frac{P_{elec,1}- P_{elec,2} (\frac{\varepsilon_2}{\varepsilon_1})}{A_s \frac{T - T_{\infty}} {(\frac{\varepsilon_2}{\varepsilon_1} - 1)}}\] From the previous part of the exercise, we know that \(A_s = 0.0201\text{ m}^2\). Plug in the values given for this problem: \[h = \frac{9.7 - 5.67 (\frac{0.1}{0.8})}{0.0201 \frac{77 - 17}{(0.125 - 1)}} = \frac{9.7- 0.709}{0.0201 \times 60} = 7.63\mathrm{~W/m^2K}\] So, the convection coefficient for Configuration B is 7.63 W/m²K.
05

Determine the temperature of surroundings

Now, let's find the temperature of the surroundings (\(T_{\text {sur}}\)). Re-examine the previous equation: \[Q_{conv,i} = h A_{s,i} (T - T_{\infty})\] \[Q_{rad,i} = \varepsilon_i \sigma A_{s,i} (T^4 - T_{\text {sur}}^4)\] To find \(T_{\text {sur}}\), we will need to solve for \(Q_{rad, 1}\) using: \[P_{elec, 1} = Q_{conv, 1} + Q_{rad, 1}\] \[Q_{rad, 1} = P_{elec, 1} - Q_{conv, 1}\] Plug in known values along with our calculated \(h\) and surface area: \[Q_{rad, 1} = 9.7 - (7.63 \times 0.0201 (77 - 17)) = 1.53\mathrm{~W}\] Now, we can rearrange the expression for \(Q_{rad, 1}\) to find \(T_{\text {sur}}\): \[T_{\text {sur}} = \sqrt[4]{\frac{Q_{rad,1}}{\varepsilon_1 \sigma A_s} + T^4}\] Plug in known values and the calculated \(Q_{rad, 1}\): \[T_{\text {sur}} = \sqrt[4]{\frac{1.53}{0.8 \times 5.67 \times 10^{-8} \times 0.0201} + 77^4} = 285.67\text{K}\] Convert the temperature of surroundings back to Celsius: \[T_{\text {sur}}^{\circ}C = 285.67\text{K} - 273.15 = 12.52^{\circ}\text{C}\] So, the temperature of the surroundings for Configuration B is 12.52°C.

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Key Concepts

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

Stefan-Boltzmann Law
The Stefan-Boltzmann Law is a principle in physics that describes how a body emits thermal radiation. It states that the power radiated per unit area of a surface is proportional to the fourth power of the temperature of the body. Mathematically, this can be expressed as \[Q_{rad} = \varepsilon \sigma A_s (T^4 - T_{\infty}^4)\]where:
  • \(\varepsilon\) is the emissivity of the surface, representing how well it emits thermal radiation compared to a perfect black body.
  • \(\sigma\) is the Stefan-Boltzmann constant, approximately \(5.67 \times 10^{-8} \ \frac{\text{W}}{\text{m}^2 \text{K}^4}\).
  • \(A_s\) is the surface area of the body through which radiation occurs.
  • \(T\) is the absolute temperature of the body in Kelvin.
  • \(T_{\infty}\) is the absolute temperature of the surroundings in Kelvin.
In the context of the exercise, the law helps determine the portion of heat transfer that occurs through radiation, which is critical for calculating the remaining heat transferred via convection.
emissivity
Emissivity (\(\varepsilon\)) is a material property that quantifies a surface's efficiency in emitting thermal radiation. It is dimensionless and ranges from 0 to 1, where 1 indicates a perfect black body that emits the maximum possible radiation and 0 means the body does not emit radiation at all. Most real-world materials have emissivity values between these extremes. Factors affecting emissivity include the material's surface roughness, coating, and temperature. For example, in the exercise, two different materials are used in Configuration B at different emissivities to accommodate unknown temperature conditions. The higher the emissivity, the greater the heat lost as radiation. Knowing the emissivity is essential when analyzing heat transfer problems as it influences the amount of energy that is radiated compared to what is absorbed. Understanding emissivity is necessary to solve problems involving combined modes of heat transfer, like radiation and convection.
convection coefficient
The convection coefficient (\(h\)) is a parameter that characterizes the heat transfer between a solid surface and a fluid (such as air or water) moving over the surface. It is usually expressed in \(\text{W/m}^2\text{K}\) and depends on several factors such as the fluid's properties, the flow regime, surface roughness, and temperature difference between the surface and the fluid. In the given exercise, the convection coefficient is crucial to calculate the convective heat transfer part. When direct calculations are made using configurations A and B, this coefficient provides insights into how efficiently heat is being removed from the disk's surface by convection compared to other modes of heat transfer. This is determined using the relationship:\[Q_{\text{conv}} = h A_s (T - T_{\infty})\] Meaning that the higher the convection coefficient, the more efficient the convective heat transfer process is. Comprehension of this concept helps in designing systems where temperature control is vital.
heat transfer rate
The heat transfer rate is a measure of the amount of heat energy transferred per unit time. In thermal systems, it indicates how effectively heat moves from one body or medium to another. It can occur via conduction, convection, or radiation.For convection, the heat transfer rate is typically calculated with:\[Q_{\text{conv}} = P_{\text{elec}} - Q_{\text{rad}}\] This formula illustrates that any residual heat, after radiation is accounted for, is assumed to be transferred through convection. Identifying and calculating heat transfer rates allows engineers and scientists to optimize thermal systems for energy efficiency and control measures. In practical applications like those found in the exercise, understanding how the heat is distributed can lead to better system designs and improve temperature control methodologies.

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Most popular questions from this chapter

During a winter day, the window of a patio door with a height of \(1.8 \mathrm{~m}\) and width of \(1.0 \mathrm{~m}\) shows a frost line near its base. The room wall and air temperatures are \(15^{\circ} \mathrm{C}\). (a) Explain why the window would show a frost layer at the base rather than at the top. (b) Estimate the heat loss through the window due to free convection and radiation. Assume the window has a uniform temperature of \(0^{\circ} \mathrm{C}\) and the emissivity of the glass surface is \(0.94\). If the room has electric baseboard heating, estimate the corresponding daily cost of the window heat loss for a utility rate of \(0.18 \mathrm{\$} / \mathrm{kW} \cdot \mathrm{h}\).

\(\mathbf{9 . 1 0 3}\) It has been proposed to use large banks of rechargeable, lithium ion batteries to power electric vehicles. The cylindrical batteries, each of which is of radius \(r_{i}=9 \mathrm{~mm}\) and length \(L=65 \mathrm{~mm}\), undergo exothermic electrochemical reactions while being discharged. Since excessively high temperatures damage the batteries, it is proposed to encase them in a phase change material that melts when the batteries discharge (and resolidifies when the batteries are charged; charging is associated with an endothermic electrochemical reaction). Consider the paraffin of Problems \(8.47\) and \(9.57\). (a) At an instant in time during the discharge of a battery, liquid paraffin occupies an annular region of outer radius \(r_{o}=19 \mathrm{~mm}\) around the battery, which is generating \(\dot{E}_{g}=1 \mathrm{~W}\) of thermal energy. Determine the surface temperature of the battery. (b) At the time of interest in part (a), what is the rate at which the liquid annulus radius is increasing? (c) Plot the battery surface temperature versus the outer radius of the liquid-filled annulus. Explain the relative insensitivity of the battery surface temperature to the size of the annulus for \(15 \mathrm{~mm} \leq\) \(r_{o} \leq 30 \mathrm{~mm}\).

A vertical, double-pane window, which is \(1 \mathrm{~m}\) on a side and has a \(25-\mathrm{mm}\) gap filled with atmospheric air, separates quiescent room air at \(T_{\infty, i}=20^{\circ} \mathrm{C}\) from quiescent ambient air at \(T_{\infty, o}=-20^{\circ} \mathrm{C}\). Radiation exchange between the window panes, as well as between each pane and its surroundings, may be neglected. (a) Neglecting the thermal resistance associated with conduction heat transfer across each pane, determine the corresponding temperature of each pane and the rate of heat transfer through the window. (b) Comment on the validity of neglecting the conduction resistance of the panes if each is of thickness \(L_{p}=6 \mathrm{~mm}\).

A solar collector design consists of an inner tube enclosed concentrically in an outer tube that is transparent to solar radiation. The tubes are thin walled with inner and outer diameters of \(0.10\) and \(0.15 \mathrm{~m}\), respectively. The annular space between the tubes is completely enclosed and filled with air at atmospheric pressure. Under operating conditions for which the inner and outer tube surface temperatures are 70 and \(30^{\circ} \mathrm{C}\), respectively, what is the convective heat loss per meter of tube length across the air space?

Consider a large vertical plate with a uniform surface temperature of \(130^{\circ} \mathrm{C}\) suspended in quiescent air at \(25^{\circ} \mathrm{C}\) and atmospheric pressure. (a) Estimate the boundary layer thickness at a location \(0.25 \mathrm{~m}\) measured from the lower edge. (b) What is the maximum velocity in the boundary layer at this location and at what position in the boundary layer does the maximum occur? (c) Using the similarity solution result, Equation \(9.19\), determine the heat transfer coefficient \(0.25 \mathrm{~m}\) from the lower edge. (d) At what location on the plate measured from the lower edge will the boundary layer become turbulent?

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