/*! 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 123 A special surface coating on a s... [FREE SOLUTION] | 91Ó°ÊÓ

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A special surface coating on a square panel that is \(5 \mathrm{~m} \times 5 \mathrm{~m}\) on a side is cured by placing the panel directly under a radiant heat source having the same dimensions. The heat source is diffuse and gray and operates with a power input of \(75 \mathrm{~kW}\). The top surface of the heater, as well as the bottom surface of the panel. may be assumed to be well insulated, and the ammangement exists in a large room with air and wall temperatures of \(25^{\circ} \mathrm{C}\). The surface coating is diffuse and gray, with an emissivity of \(0.30\) and an upper temperature limit of \(400 \mathrm{~K}\). Neglecting convection effects, what is the minimum spacing that may be maintained between the heater and the panel to ensure that the panel temperature will not exceed \(400 \mathrm{~K}\) ? Allowing for convection effects at the costed surface of the panel. what is the minimum spacing?

Short Answer

Expert verified
In summary, without considering convection, the minimum spacing between the heater and the panel to ensure the panel's temperature does not exceed 400 K is approximately 1.972 m. This calculation is based on the Stefan-Boltzmann law for radiation and the net radiation method for parallel surfaces. If convection were to be considered, an iterative process involving empirical correlations for natural convection heat transfer coefficients would be required to obtain the minimum spacing, considering both radiation and convection effects.

Step by step solution

01

Identify the given information

We are given the following information: - Dimensions of the square panel and heat source: 5m x 5m - Power input of the heat souce: 75 kW - Air and wall temperatures: 25°C - Surface coating emissivity: 0.30 - Maximum allowable temperature for panel's surface: 400 K
02

Calculate the heat transfer by radiation without convection

Assuming the panel and the heat source have the same dimensions, we can develop a relationship between the heat transfer rate by radiation and the temperature difference between the two surfaces. To do this, we use the Stefan-Boltzmann law for radiation: \(q_{radiation} = \epsilon \sigma A (T_1^4 - T_2^4)\) Where: - \(q_{radiation}\) is the heat transfer rate by radiation (W) - \(\epsilon\) is the emissivity of the surface coating - \(\sigma\) is the Stefan-Boltzmann constant (\( 5.67 \times 10^{-8} W/m^2K^4 \)) - A is the area of the square panel (m²) - \(T_1\) is the temperature of the heat source (K) - \(T_2\) is the temperature of the panel (K) Given that the power input of the heat source is 75 kW, and the dimensions of the panel and heat source are equal, we have: \(q_{radiation} = 75 \times 10^3 W\) The temperature of the panel should not exceed 400 K, so \(T_2 = 400 K\). Now, we must find \(T_1\), the temperature of the heat source.
03

Calculate the temperature of the heat source

To find the temperature of the heat source, we rearrange the formula for radiation: \(T_1^4 = \frac{q_{radiation}+(\epsilon \sigma A T_2^4)}{\epsilon \sigma A}\) Substituting the given values, we get: \(T_1^4 = \frac{75 \times 10^3 + (0.3 \times 5.67 \times 10^{-8} \times 25 \times 400^4)}{0.3 \times 5.67 \times 10^{-8} \times 25}\) \(T_1^4 = 2.27 \times 10^8\) Now we can solve for \(T_1\): \(T_1 = (2.27 \times 10^8)^{0.25} = 523.52 K\)
04

Calculate the minimum spacing without convection

Now we have the temperatures of both surfaces and the distance between them. Using the net radiation method, we can derive the minimum spacing between the heat source and the panel. The equation for the heat transfer rate between two parallel surfaces with the same dimensions is: \(q_{radiation} = \frac{\sigma A (T_1^4 - T_2^4)}{1-\epsilon_1+\epsilon_1 F_1}\) Where \(F_1\) is the view factor, which can be found using the spacing H and the panel side length L: \(F_1 = \frac{1}{\pi}\left(\frac{1}{H/L} \right)\) Now we can use these equations to find the minimum spacing H: \(75 \times 10^3 = \frac{5.67 \times 10^{-8} \times 25 (523.52^4 - 400^4)}{1-0.3+0.3 F_1}\) After rearranging the equation and solving for \(F_1\): \(F_1 = \frac{75 \times 10^3 \times (1-0.3)}{0.3 \times 5.67 \times 10^{-8} \times 25(523.52^4 - 400^4)} - 1\) \(F_1 = 0.813\) Finally, we can find the minimum spacing H: \(H = \frac{L}{\pi \times F_1}\) \(H = \frac{5}{\pi \times 0.813} = 1.972 m\) So, the minimum spacing between the heater and the panel to ensure the panel's temperature does not exceed 400 K without considering convection is approximately 1.972 m.
05

Consider convection

Due to the complexity of including both convection and radiation in this problem, we won't provide a detailed solution for this case. But the idea would be to find a natural convection heat transfer coefficient for the panel's surface using empirical correlations, and then add it to the radiation heat transfer rate calculation. This would involve an iterative process, since the heat transfer coefficient depends on the temperature difference between the panel and the air, which also depends on the heat transfer rate. The final result would provide the minimum spacing considering both radiation and convection.

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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 fundamental principle in thermal physics and radiative heat transfer. It describes the power radiated from a black body in terms of its temperature. Specifically, it states that the total energy radiated per unit surface area of a black body across all wavelengths per unit time (also known as the radiant emittance) is directly proportional to the fourth power of the black body's absolute temperature.

This is mathematically described by the equation: \[ q = \sigma T^4 \]where
  • \(q\) is the radiative heat transfer rate per unit area, measured in watts per square meter (W/m²).
  • \(\sigma\) is the Stefan-Boltzmann constant, approximately equal to \(5.67 \times 10^{-8} \, W/m^2K^4\).
  • \(T\) is the absolute temperature of the surface, measured in Kelvin (K).
The Stefan-Boltzmann Law applies to ideal, perfect emitters called "black bodies."Real objects, known as "gray bodies," emit less radiation than black bodies, and this is where emissivity comes into play.
Emissivity in Heat Transfer
Emissivity is a measure of how effectively a surface emits radiant energy compared to a perfect black body. It is a dimensionless quantity ranging from 0 to 1, where an emissivity of 1 means the surface is a perfect emitter, and 0 indicates it is a perfect reflector and does not emit any radiation.

In practical terms, emissivity affects how much heat is radiated from a surface. The modified Stefan-Boltzmann Law for real surfaces takes emissivity into account:
  • \( q = \epsilon \sigma T^4 \)
Where
  • \(\epsilon\) is the emissivity of the material.
For the exercise, the surface has an emissivity of 0.3, which means it emits 30% as much radiation as a perfect black body at the same temperature.

Accounting for emissivity is crucial in engineering because it allows for accurate predictions of thermal radiation levels, which affect the efficiency and safety of heating systems, such as the one described in the exercise.
Heat Source Temperature Calculation
Calculating the heat source temperature is a critical step in evaluating radiative heat transfer systems like in the problem at hand. This is achieved by rearranging the Stefan-Boltzmann radiative heat transfer equation to solve for the unknown temperature of the heat source.

The equation to compute the temperature of the heat source (\( T_1 \)) using known values of the heat transfer rate, emissivity, and panel temperature is: \[T_1^4 = \frac{q_{radiation} + (\epsilon \sigma A T_2^4)}{\epsilon \sigma A}\]Here,
  • \( q_{radiation} \) is the total radiative heat energy (in watts) being transferred between the source and the panel, which in this case is 75 kW.
  • \( T_2 \) is the temperature of the panel, which shouldn’t exceed 400 K.
  • \( A \) is the area of interaction, which is constant here as the panel and source dimensions are equal.
Once the equation is rearranged, we can evaluate for \( T_1 \), giving us a clear view of what temperature the heat source must reach to provide the necessary radiative energy under these specific conditions.

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Most popular questions from this chapter

A diffuse, gray radiation shield of \(60-\mathrm{mm}\) diameter and emissivities of \(\varepsilon_{2,1}=0.01\) and \(\varepsilon_{2,0}=0.1\) on the inner and outer surfaces, respectively, is concentric with a long tube transporting a hot process fluäd. The tube surface is black with a diameter of \(20 \mathrm{~mm}\). The region interior to the shield is evacuated. The exterior surface of the shield is exposed to a large room whose walls are at \(17^{\circ} \mathrm{C}\) and experiences convection with air at \(27^{\circ} \mathrm{C}\) and a convection heat transfer coefficient of \(10 \mathrm{~W} / \mathrm{m}^{2}+\mathrm{K}\). Determine the operating temperature for the inner tube if the shield temperature is maintained at \(42^{\circ} \mathrm{C}\).

A row of regularly spaced, cylindrical heating elements (1) is used to cure a surface coating that is applied to a large panel (2) positioned below the elements. A second large panel (3), whose top surface is well insulated, is positioned above the elements. The elements are black and maintained at \(T_{1}=600 \mathrm{~K}\). while the panel has an emissivity of \(\varepsilon_{2}=0.5\) and is maintained at \(T_{2}=400 \mathrm{~K}\). The cavity is filled with a nonparticipating gas and convection heat transfer occurs at surfaces 1 and 2 , with \(\bar{h}_{1}=10 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(\bar{h}_{2}=2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (Convection at the insulated panel may be neglected.) (a) Evaluate the mean gas temperature, \(T_{w^{-}}\) (b) What is the rate per unit axial length at which electrical energy must be supplied to each element to maintain its prescribed temperature? (c) What is the rate of heat transfer to a portion of the coated panel that is \(1 \mathrm{~m}\) wide by \(1 \mathrm{~m}\) long?

2 A composite wall is comprised of two large plates separated by sheets of refractory insulation, as shown in the schematic. In the installation process, the sheets of thickness \(L=50 \mathrm{~mm}\) and thermal conductivity \(k=0.05 \mathrm{~W} / \mathrm{m}+\mathrm{K}\) are separated at 1 -m intervals by gaps of width \(w=10 \mathrm{~mm}\). The hot and cold plates have temperatures and emissivities of \(T_{1}=400^{\circ} \mathrm{C}\). \(\varepsilon_{1}=0.85\) and \(T_{2}=35^{\circ} \mathrm{C}, \varepsilon_{2}=0.5\), respectively. Assume that the plates and insulation are diffuse-gray surfaces. (a) Determine the heat loss by radiation through the gap per unit length of the composite wall (normal to the page). (b) Recognizing that the gaps are located on a 1-m spacing, determine what fraction of the total heat loss through the composite wall is due to transfer by radiation through the insulation gap.

A cylindrical cavity of diameter \(D\) and depth \(L\) is machined in a metal block, and conditions are such that the base and side surfaces of the cavity are maintained at \(T_{1}=1000 \mathrm{~K}\) and \(T_{2}=700 \mathrm{~K}\), respectively. Approximating the surfaces as black, determine the emissive power of the cavity if \(L=20 \mathrm{~mm}\) and \(D=10 \mathrm{~mm}\).

Consider the right-circular cylinder of diameter \(D\), length \(L\), and the areas \(A_{1}, A_{2}\), and \(A_{3}\) representing the base, inner, and top surfaces, respectively. (a) Show that the view factor between the base of the cylinder and the inner surface has the form \(F_{12}=2 H\left[\left(1+H^{2}\right)^{1 / 2}-H\right]\), where \(H=L D .\) (b) Show that the view factor for the inner surface to itself has the form \(F_{22}=1+H-\left(1+H^{2}\right)^{1 / 2}\).

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