/*! 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 109 Options for thermally shielding ... [FREE SOLUTION] | 91Ó°ÊÓ

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Options for thermally shielding the top ceiling of a large furnace include the use of an insulating material of thickness \(L\) and thermal conductivity \(k\), case (a), or an air space of equävalent thickness formed by installing a steel sheet above the ceiling, case \((b)\). (a) Develop mathematical models that could be used to assess which of the two approaches is better. In both cases the interior surface is maintained at the same temperature, \(T_{s,}\) and the ambient air and surroundings are at equivalent temperatures \(\left(T_{w}=T_{\text {ue }}\right)\). (b) If \(k=0.090 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, L=25 \mathrm{~mm}, h_{a}=25\) W/ \(\mathrm{m}^{2} \cdot \mathrm{K}\), the surfaces are diffuse and gray with \(\varepsilon_{i}=\varepsilon_{o}=0.50, T_{s u}=900 \mathrm{~K}\), and \(T_{w}=T_{\mathrm{ar}}=\) \(300 \mathrm{~K}\), what is the outer surface temperature \(T_{\text {a }}\) and the heat loss per unit surface area associated with each option? (c) For each case, assess the effect of surface radiative properties on the outer surface temperature and the heat loss per unit area for values of

Short Answer

Expert verified
(a) The mathematical models for each case are as follows: Case (a): Insulating Material \(q_{total} = q_{c} + q_{r} = k\frac{T_{s} - T_a}{L} + \varepsilon \sigma (T_{s}^4 - T_a^4)\) Case (b): Air Gap \(q_{total} = q_{c} + q_{r} = h_a(T_{s} - T_a) + \varepsilon \sigma (T_{s}^4 - T_a^4)\) (b) Using the given values, we can calculate the heat loss and outer surface temperature for both cases. Case (a): \(T_{a}\approx 451.92\text{ K}\) and \(q_{total}\approx 1848.94\text{ W/m}^2\) Case (b): \(T_{a}\approx 718.69\text{ K}\) and \(q_{total}\approx 4528.58\text{ W/m}^2\) (c) Evaluating the impact of surface radiative properties on outer surface temperature and heat loss shows that increasing emissivity reduces heat loss and outer surface temperature in both cases, enhancing their thermal shielding performance.

Step by step solution

01

(a) Mathematical Models for Both Cases

Case (a): Insulating Material We can calculate the heat transfer through the insulating material by considering conduction heat transfer through the material and radiation heat transfer between the two surfaces. First, we have to find the heat flux due to conduction and radiation. For conduction, we will use Fourier's law of heat conduction: \(q_{c} = k\frac{T_{s} - T_a}{L}\) For radiation, we will use the Stefan-Boltzmann radiation law: \(q_{r} = \varepsilon \sigma (T_{s}^4 - T_a^4)\) Total heat flux through the insulating material will be: \(q_{total} = q_{c} + q_{r}\) Since we need the mathematical model for both cases, we can use heat-transfer coefficients to generalize the equations for conduction and radiation heat fluxes. Case (b): Air Gap For the air gap, we would consider both convective heat transfer between the surfaces, and radiative heat transfer between the surfaces. Convective heat transfer: \(q_{c} = h_a(T_{s} - T_a)\) Radiative heat transfer: \(q_{r} = \varepsilon \sigma (T_{s}^4 - T_a^4)\) The total heat loss through the air gap would be: \(q_{total} = q_{c} + q_{r}\)
02

(b) Heat Loss and Outer Surface Temperature for Both Cases

Given values are: \(k = 0.090 \;\text{W/m·K}\), \(L = 0.025 \;\text{m}\), \(h_{a} = 25\;\text{W/m}^2\cdot\text{K}\), \(\varepsilon_{i} = \varepsilon_{o} = 0.50\), \(T_{s} = 900\;\text{K}\), \(T_{w} = T_{\text{ar}} = 300\;\text{K}\). Case (a): Insulating Material -> Solve for heat flux due to conduction \(q_{c} = k\frac{T_{s} - T_a}{L}\), \(q_{c} = 0.09\frac{900 - T_a}{0.025}\), -> Solve for heat flux due to radiation \(q_{r} = \varepsilon \sigma (T_{s}^4 - T_a^4)\), \(q_{r} = 0.50 \sigma (900^4 - T_a^4)\), -> Add the heat transfer rates and solve for \(T_a\) and \(q_{total}\): For Case (b): Air Gap -> Solve for heat flux due to convection \(q_{c} = h_a(T_{s} - T_a)\), \(q_{c} = 25(900 - T_a)\), -> Solve for heat flux due to radiation \(q_{r} = \varepsilon \sigma (T_{s}^4 - T_a^4)\), \(q_{r} = 0.50 \sigma (900^4 - T_a^4)\), -> Add the heat transfer rates and solve for \(T_a\) and \(q_{total}\):
03

(c) Analyzing Effects of Surface Radiative Properties for Both Cases

To analyze the effects of surface radiative properties on outer surface temperature and heat loss per unit area, we'll vary the emissivity of the surfaces and use the previous equations for total heat flux and outer surface temperature in each case. By investigating the relationship between emissivity and these quantities, we can evaluate how the surface radiative properties impact the performance of each thermal shielding option.

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Key Concepts

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

Heat Transfer
Heat transfer is the process of energy moving from a hotter object to a cooler one. It's essential in many applications, such as designing structures like furnaces, where managing heat is crucial. There are three primary ways heat is transferred, which include conduction, convection, and radiation. Each mechanism plays a significant role in how thermal insulation models are developed and assessed.

In the scenario of thermal insulation for a furnace, heat transfer determines how effective an insulating material or air gap is between the interior and exterior surfaces. Knowing how heat is transferred can help in selecting the most appropriate insulation strategy, such as using a solid insulating material or creating an air space. Understanding and calculating the rate of heat transfer allows for better design and improved energy efficiency.
Thermal Conductivity
Thermal conductivity is a measure of a material's ability to conduct heat. Materials with high thermal conductivity, like metals, transfer heat rapidly, while insulating materials with low thermal conductivity slow down heat transfer. This property is vital when choosing materials for thermal insulation.

In the furnace example, knowing the thermal conductivity of the insulating material is crucial. It allows you to calculate the rate of heat conduction using Fourier's law, given by the formula:\[ q_{c} = k\frac{T_{s} - T_a}{L} \]where
  • \(q_c\) is the conduction heat flux,
  • \(k\) is the thermal conductivity,
  • \(T_{s}\) and \(T_a\) are the surface and ambient temperatures, respectively,
  • \(L\) is the thickness of the material.
By applying this calculation, you are able to determine how effective different materials are for minimizing heat loss.
Radiative Heat Transfer
Radiative heat transfer involves the emission and absorption of thermal radiation, which is energy emitted by matter based on its temperature. Unlike conduction and convection, radiation does not require a medium, as it can occur in a vacuum.

The effectiveness of radiative heat transfer is determined by a surface's emissivity, a measure of how efficiently a surface emits thermal radiation. In the exercise, surfaces are considered diffuse and gray with an emissivity of 0.50.

The heat flux due to radiation is calculated using the Stefan-Boltzmann law:\[ q_{r} = \varepsilon \sigma (T_{s}^4 - T_a^4) \]where
  • \(q_r\) is the radiative heat flux,
  • \(\varepsilon\) is the emissivity,
  • \(\sigma\) is the Stefan-Boltzmann constant,
  • \(T_{s}\) and \(T_a\) are the temperatures of the surfaces.
Radiative heat loss can significantly affect the choice of thermal insulation strategies, especially when the temperatures are high.
Convection
Convection is the transfer of heat through a fluid (like air or water) moving over a surface. There are two types, natural and forced, depending on whether the fluid movement is due to density differences or external forces.

In the case of the furnace, if an air gap is used, convective heat transfer becomes vital. It is determined by the heat-transfer coefficient, \(h_a\), and the temperature difference between the surfaces. Convective heat transfer can be calculated using:\[ q_{c} = h_a (T_{s} - T_a) \]where
  • \(q_c\) is the convective heat flux,
  • \(h_a\) is the heat transfer coefficient,
  • \(T_s\) and \(T_a\) are the temperatures of the surfaces.
Understanding convection helps in determining how adding an air layer will impact the thermal protection of the furnace, influencing whether it is more economical or effective than traditional solid insulation. Adjusting the air gap's properties and characteristics can help improve insulation performance.

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Most popular questions from this chapter

A row of regularly spaced, cylindrical heating elements is used to maintain an insulated furnace wall at \(500 \mathrm{~K}\). The opposite wall is at a uniform temperature of \(300 \mathrm{~K}\). The insulated wall experiences convection with air at \(450 \mathrm{~K}\) and a convection coefficient of \(200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Assuming the walls and elements are black, estimate the required operating temperature for the elements.

The lower side of a \(400-\mathrm{mm}\)-diameter disk is heated by an electric furnace, while the upper side is exposed to quiescent, ambient air and sumoundings at \(300 \mathrm{~K}\). The radiant furnace (negligible convection) is of circular construction with the bottoen surface \(\left(\alpha_{1}-0.6\right)\) and cylindrical side surface \(\left(\varepsilon_{1}=1.0\right)\) maintained af \(T_{1}=T_{2}=500 \mathrm{~K}\). The surface of the disk facing the radiant furnace is black \(\left(\varepsilon_{d, 1}=1.0\right)\). while the upper surface has an emissivity of \(\varepsilon_{d, 2}=0.8\). Assume the plate and furnace surfaces to be diffuse and gray. (a) Determine the net heat transfer rate to the disk, \(q_{\text {nated, when }} T_{d}=400 \mathrm{~K}\). (b) Plot \(q_{\text {netd as a }}\) a function of the disk temperature for \(300 \leq T_{a} \leq 500 \mathrm{~K}\), with all other conditions remaining the same. What is the steady-state temperature of the disk?

A cylindrical furnace for heat-treating materials in a spacecraft environment has a \(90-\mathrm{mm}\) diameter and an overall length of \(180 \mathrm{~mm}\). Heating elements in the 135 -mm-long section (1) maintain a refractory lining of \(\varepsilon_{1}=0.8\) at \(800^{\circ} \mathrm{C}\). The linings for the bottom (2) and upper (3) sections are made of the same refractory material, but are insulated.

An electrically heated sample is maintained at a surface temperature of \(T_{s}=500 \mathrm{~K}\). The sample coating is diffuse but spectrally selective, with the spectral emissivity distribution shown schematically. The sample is irradiated by a furnace located coaxially at a distance of \(L_{\mathrm{s}}=750 \mathrm{~mm}\). The furnace has isothermal walls with an emissivity of \(s_{f}=0.7\) and a uniform temperature of \(T_{f}-3000 \mathrm{~K}\). A radiation detector of area \(A_{d}=8 \times 10^{-5} \mathrm{~m}^{2}\) is positioned at a distance of \(L_{\mathrm{dd}}=1.0 \mathrm{~m}\) from the sample along a direction that is \(45^{\circ}\) from the sample normal. The detector is sensitive to spectral radiant power only in the spectral region from 3 to \(5 \mu \mathrm{m}\). The sample surface experiences convection with a gas for which \(T_{\infty}=300 \mathrm{~K}\) and \(h=20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The surroundings of the sample mount are large and at a uniform temperature of \(T_{\text {sur }}=300 \mathrm{~K}\). (a) Determine the electrical power, \(P_{c}\), required to maintain the sample at \(T_{s}=500 \mathrm{~K}\). (b) Considering both emission and reflected irradiation from the sample, determine the radiant power that is incident on the detector within the spectral region from 3 to \(5 \mu \mathrm{m}\).

A heat flux gage of 4-mm diameter is positioned normal to and \(1 \mathrm{~m}\) from the 5 -mm-diameter aperture of a blackbody furnace at \(1000 \mathrm{~K}\). The diffuse, gray cover shield \((\varepsilon=0.2)\) of the furnace has an outer diameter of \(100 \mathrm{~mm}\) and its temperature is \(350 \mathrm{~K}\). The furnace and gage are located in a large room whose walls have an emissivity of \(0.8\) and are at \(300 \mathrm{~K}\). (a) What is the irradiation on the gage, \(G_{g}\) (W/m²), considering only emission from the aperture of the furnace? (b) What is the irradiation on the gage due to radiation from the cover and aperture?

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