/*! 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 125 A long furnace with a \(2 \mathr... [FREE SOLUTION] | 91Ó°ÊÓ

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A long furnace with a \(2 \mathrm{~m}-\) square cross section has three refractory walls, and one wall cooled to \(400 \mathrm{~K}\). Combustion gases at \(1200 \mathrm{~K}\) flow through the furnace. The cooled wall is gray, with an emittance of \(0.7\), and the gases can be modeled as isothermal and gray, with a total absorption coefficient \(\kappa=0.15 \mathrm{~m}^{-1}\). Determine the radiant heat transfer to the cooled wall.

Short Answer

Expert verified
The radiant heat transfer to the cooled wall is approximately 10,852.18 W/m².

Step by step solution

01

Understand the Problem Setup

In this problem, we have a long furnace with a square cross-section. Three of the walls are refractory, meaning they are not actively part of the thermal transfer equation we're focusing on. Our interest is in the cooled wall which is also gray, meaning it has a consistent emittance value of 0.7, and is at a fixed temperature of 400 K. The combustion gases inside the furnace can be treated as an isothermal medium at 1200 K, with a given absorption coefficient. We need to calculate the radiant heat transfer to this cooled wall.
02

Apply the Radiant Heat Transfer Equation

The radiant heat transfer to the cooled wall can be calculated using the equation for radiative transfer with a gray gas:\[q = \kappa \cdot (G - E)\]where \( G \) is the incident radiation on the wall and \( E \) is the emitted radiation from the wall. Both \( G \) and \( E \) can be calculated using Stefan-Boltzmann law and parameters given in the problem.
03

Calculate Emitted Radiation

The emitted radiation, \( E \), from the wall is given by:\[E = \epsilon \cdot \sigma \cdot T_w^4\]where \( \epsilon = 0.7 \) is the emittance, \( \sigma = 5.67 \times 10^{-8} \mathrm{~W/m^2 \, K^4} \) is the Stefan-Boltzmann constant, and \( T_w = 400 \, \mathrm{K} \) is the wall temperature. This evaluates to:\[E = 0.7 \times 5.67 \times 10^{-8} \times (400)^4 = 1146.72 \, \text{W/m}^2\]
04

Calculate Incident Radiation

Incident radiation, \( G \), from the gas can be calculated using the temperature of the gases:\[G = \sigma \cdot T_g^4\]where \( T_g = 1200 \, \mathrm{K} \). This calculates to:\[G = 5.67 \times 10^{-8} \times (1200)^4 = 73,570.56 \, \text{W/m}^2\]
05

Solve for Net Radiant Heat Transfer

Now substitute \( G \) and \( E \) back into the radiant heat transfer equation:\[q = \kappa \cdot (G - E) = 0.15 \times (73,570.56 - 1146.72) = 10,852.18 \, \text{W/m}^2\]This result represents the net radiant heat transfer to the cooled wall, considering the absorption coefficient.

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Key Concepts

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

Emittance
Emittance is a crucial concept in radiant heat transfer. It describes how effectively a surface emits thermal radiation compared to an ideal black body. In the original exercise, we consider the emittance of a gray wall, which has a fixed value of 0.7.
This means the wall emits 70% of the thermal radiation that a perfect black body would at the same temperature.Understanding emittance helps us determine how much heat the wall itself emits. This emitted radiation depends on three key factors:
  • The emittance ( 80.7 in the exercise) of the material.
  • The Stefan-Boltzmann constant ( 85.67 \times 10^{-8} \, \text{W/m}^2 \, \text{K}^4).
  • The fourth power of the wall's absolute temperature (400 K in the exercise).
These factors combine in the equation: \[ E =  80.7 imes 5.67 \times 10^{-8} \times 400^4 \]Emittance is especially important when comparing the heat radiation of different materials or surfaces, as each has its own unique ability to emit thermal energy.
Stefan-Boltzmann Law
The Stefan-Boltzmann Law is central to calculating radiant energy emissions from a surface. This law states that the power radiated per unit area of a black body is proportional to the fourth power of its temperature in Kelvin. Mathematically, it is expressed as:\[ E =  8 8\sigma \times T^4 \]Here, \( E \) represents the emissive power, \(  8\sigma \) is the Stefan-Boltzmann constant, and \( T \) is the absolute temperature in Kelvin.In the original exercise, the Stefan-Boltzmann Law is crucial in calculating both the emitted and incident radiation. For a gray body, like our wall with emittance 0.7, we modify the equation to:\[ E =  8\epsilon \times  8\sigma \times T_w^4 \]Using this equation, we derived the emitted radiation from the cooled wall at 400 K. The law thus allows determining how much radiant energy is moving toward or away from a surface, considering both the surface temperature and its emittance.
Absorption Coefficient
The absorption coefficient is a measure of how readily a material or medium absorbs radiation. It plays a vital role in radiant heat transfer involving gases or fluids. An absorption coefficient is often specific to the type of gas and its properties.In the given exercise, gases flowing through the furnace have an absorption coefficient, \( \kappa \), of 0.15 \( \, \text{m}^{-1} \). This value indicates how effectively the combustion gases absorb the radiant energy before it reaches the cooled wall.The radiant heat transfer to the wall is determined using the equation:\[ q = \kappa \times (G - E) \]This equation considers both the incident radiation, \( G \), which is the energy radiation from the gases at 1200 K, and the emitted radiation, \( E \), from the cooled wall.
An understanding of the absorption coefficient helps predict the net heat transferred by effectively accounting for the radiative interactions in the thermal system, balancing what is lost in emission with what is absorbed.

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Most popular questions from this chapter

A kiln has an average inside surface temperature of \(2330 \mathrm{~K}\) and has a small \(15 \times\) \(15 \mathrm{~cm}\) square opening in its \(20 \mathrm{~cm}\)-thick walls. If the sides of the opening can be assumed to be adiabatic, determine the rate of radiant energy loss through the opening.

A \(100 \mathrm{~W}, 10 \mathrm{~cm}\)-diameter disk heater is placed parallel to, and \(5 \mathrm{~cm}\) from, a 10 \(\mathrm{cm}\)-diameter disk receiver in an evacuated chamber. The backs of both disks are well insulated. If the disk surfaces have emittances of \(0.8\) and the walls of the chamber are black and maintained at \(350 \mathrm{~K}\), calculate the following quantities: (i) The heater temperature. (ii) The receiver temperature. (iii) The radiative heat transfer between the heater and receiver. (iv) The net radiative heat transfer to the chamber.

Freezing of oranges in an orchard during winter can be catastrophic to the farmer. Estimate the rate at which an \(8 \mathrm{~cm}\)-diameter orange hanging on a tree cools as a function of its temperature when the air has a temperature of \(2^{\circ} \mathrm{C}\) and a relative humidity of \(75 \%\). Assume a convective heat transfer coefficient of \(3 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\), an emittance of orange peel of \(\varepsilon_{1}=0.9\), and an emittance of surrounding leaves and grass of \(\varepsilon_{2}=1.0\). Take the shape factor for the orange to surrounding leaves and grass as \(F_{12}=0.75\), and to the sky as \(F_{13}=0.25\). Estimate the temperature of the leaves and grass by requiring that they be adiabatic with \(F_{23}=0.5\). Will the convective heating when the orange is at \(0^{\circ} \mathrm{C}\) exceed the radiative cooling? If not, will the use of fans to increase \(h_{c}\) from 3 to \(12 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\) prevent freezing? For the orange, take \(\rho=900 \mathrm{~kg} / \mathrm{m}^{3}\) and \(c_{p}=3600 \mathrm{~J} / \mathrm{kg} \mathrm{K}\). (Hint: First find \(T_{2}\) from an energy balance on unit area \(A_{2}=1\). Note that since \(A_{1} F_{12}=A_{2} F_{21}, F_{21}\) is negligible. Then find \(\dot{Q}_{1}\) and \(\left.d T_{1} / d t .\right)\)

A square room of sides \(8 \mathrm{~m}\) has a \(3 \mathrm{~m}\)-diameter radiant heating panel centrally located on the ceiling, \(3 \mathrm{~m}\) above the floor. The panel can be taken to be black and is maintained at \(60^{\circ} \mathrm{C}\). Calculate the irradiation on the floor due to the heater, at the center of the room, and in one corner.

A thermistor is used to measure the temperature of a hot-air stream in a forced-air heating system of a hospital. It is located in a \(1 \mathrm{~m}\)-square duct through which air flows at \(1.6 \mathrm{~m} / \mathrm{s}\). The thermistor can be modeled as a \(3 \mathrm{~mm}\)-diameter sphere of emittance \(0.8\) and is located inside a radiation shield in the form of a 1 \(\mathrm{cm}-\) diameter, \(5 \mathrm{~cm}\)-long tube of emittance \(0.7\) (the axis of the tube is in the flow direction). If the thermistor records a temperature of \(46.8^{\circ} \mathrm{C}\) when the duct walls are at \(43.5^{\circ} \mathrm{C}\), determine the true temperature of the air. Convective heat transfer coefficients on the thermistor and shield can be taken as \(93 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\) and \(22 \mathrm{~W} / \mathrm{m}^{2}\) \(\mathrm{K}\), respectively. (Hint: First estimate the shield temperature.)

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