/*! 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 74 The \(50-\mathrm{mm}\) peephole ... [FREE SOLUTION] | 91Ó°ÊÓ

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The \(50-\mathrm{mm}\) peephole of a large furnace operating at \(450^{\circ} \mathrm{C}\) is covered with a material having \(\tau=0.8\) and \(\rho=0\) for irradiation originating from the furnace. The material has an emissivity of \(0.8\) and is opaque to irradiation from a source at room temperature. The outer surface of the cover is exposed to surroundings and ambient air at \(27^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of \(50 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Assuming that convection effects on the inner surface of the cover are negligible, calculate the heat loss by the furnace and the temperature of the cover.

Short Answer

Expert verified
The short answer for this problem is as follows: First, find the irradiation from the furnace using the Stefan-Boltzmann law with the given temperature and tau value. Then, calculate the total emissive power of the material using its emissivity and Stefan-Boltzmann constant. Set up the radiative and convective heat transfer equations, and combine them to get the total heat transfer equation. Finally, solve for the temperature of the cover and the heat loss by the furnace using a numerical method or software tool.

Step by step solution

01

Calculate the irradiation from the furnace

First, we need to calculate the irradiation from the furnace, \(I_{furnace}\). We use the Stefan-Boltzmann law: \[ I_{furnace} = \tau \cdot \sigma \cdot T_{furnace}^4 \] where \(\tau = 0.8\) is the transmissivity of the material, \(\sigma = 5.67 \cdot 10^{-8} \ \mathrm{W/m^2K^4}\) is the Stefan-Boltzmann constant, \(T_{furnace} = 450^{\circ}\mathrm{C} + 273.15 = 723.15\ \mathrm{K}\) is the furnace temperature in Kelvin. Now, we can solve for \(I_{furnace}\): \[ I_{furnace} = 0.8 \cdot 5.67 \cdot 10^{-8} \cdot (723.15)^4 \]
02

Calculate the total emissive power of the material

Next, we need to calculate the total emissive power of the material, \(E_{material}\). We use the formula: \[ E_{material} = \epsilon \cdot \sigma \cdot T_{material}^4 \] where \(\epsilon = 0.8\) is the emissivity of the material, \(T_{material}\) is the temperature of the cover in Kelvin.
03

Set up the radiative heat transfer equation

Now, we can set up the radiative heat transfer equation: \[ q_{rad} = AI_{furnace} - AE_{material} \] where \(A\) is the area of the peephole, which we will later cancel out.
04

Set up the convection heat transfer equation

We will now set up the convection heat transfer equation: \[ q_{conv} = hA(T_{material} - T_{ambient}) \] where \(h = 50\ \mathrm{W/m^2K}\) is the convection heat transfer coefficient, \(T_{ambient} = 27^{\circ}\mathrm{C} + 273.15 = 300.15\ \mathrm{K}\) is the ambient temperature.
05

Combine the radiative and convective heat transfer equations

The total heat transfer is the sum of the radiative and convective heat transfers: \[ q_{total} = q_{rad} + q_{conv} \] Substituting the expressions from Steps 3 and 4: \[ q_{total} = A(I_{furnace} - E_{material}) + hA(T_{material} - T_{ambient}) \] Since we are interested in the total heat loss and not per unit surface area, we can divide both sides by \(A\) and cancel it out: \[ \frac{q_{total}}{A} = I_{furnace} - E_{material} + h(T_{material} - T_{ambient}) \]
06

Solve for the temperature of the cover

Now we need to solve for \(T_{material}\). First, we plug in the expression for \(E_{material}\) from Step 2: \[ \frac{q_{total}}{A} = I_{furnace} - \epsilon \sigma T_{material}^4 + h(T_{material} - T_{ambient}) \] Solve this non-linear equation for \(T_{material}\) using a numerical method or software tool. Once you have \(T_{material}\), plug it back into both the radiative and convective equations to find \(q_{rad}\) and \(q_{conv}\). Finally, calculate the total heat loss \(q_{total}\).

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Key Concepts

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

Stefan-Boltzmann Law
When dealing with heat transfer, the Stefan-Boltzmann Law is crucial as it helps us calculate the amount of thermal radiation emitted by a surface. This law states that the power radiated by a black body per unit area is directly proportional to the fourth power of the black body's absolute temperature. Mathematically, it is expressed as:\[ E = \sigma T^4 \]where:
  • \(E\) is the emissive power
  • \(\sigma = 5.67 \times 10^{-8} \, \mathrm{W/m^2K^4}\) is the Stefan-Boltzmann constant
  • \(T\) is the absolute temperature of the body in Kelvin
The use of this law is demonstrated in calculating the irradiation from the furnace. You need the temperature in Kelvin to apply it, so remember to convert from Celsius or other units to Kelvin first.
Emissivity
Emissivity is a material property that measures how effectively a surface emits thermal radiation compared to an ideal black body, which has an emissivity of 1. Real-world objects have an emissivity value between 0 and 1.
  • An emissivity close to 1 means the material is a good emitter of radiation.
  • An emissivity close to 0 means the material emits very little thermal radiation.
In the exercise, the covering material of the furnace peephole has an emissivity of 0.8. This indicates it is quite effective in emitting the thermal radiation, though not as perfect as a theoretical black body. When performing calculations involving emissive power, it is crucial to adjust the Stefan-Boltzmann Law to account for emissivity. This adjustment is done by multiplying the original equation with the emissivity \(\epsilon\), like:\[ E_{material} = \epsilon \sigma T_{material}^4 \]This formula helps in determining the total power radiated by a real material.
Convection Heat Transfer
Convection is a mode of heat transfer that occurs in fluids. It involves the bulk movement of molecules within fluids (liquids and gases) and is a major way heat is transferred in atmospheres, oceans, and within our homes.In the exercise, convection affects the outer surface of the furnace cover. The surrounding air at \(27^{\circ} \mathrm{C}\) aids in transferring heat away from the cover. Convection can be calculated using:\[ q_{conv} = hA(T_{material} - T_{ambient}) \]where:
  • \(q_{conv}\) is the heat transfer rate due to convection
  • \(h = 50 \mathrm{W/m^2K}\) is the convection heat transfer coefficient
  • \(A\) is the area
  • \(T_{material}\) and \(T_{ambient}\) are the temperatures of the material and surroundings in Kelvin
Understanding convection is key to solving this problem as it involves determining how much heat is being lost from the furnace through the process of air movement around the cover.
Radiative Heat Transfer
Radiative heat transfer occurs when thermal energy is emitted by a body due to its temperature and travels away in the form of electromagnetic waves. Unlike conduction and convection, radiation does not need a medium and can occur in a vacuum.In this problem, the furnace and the environmental factors surrounding it engage in radiative heat transfer. To determine the transfer rate:\[ q_{rad} = AI_{furnace} - AE_{material} \]This equation accounts for:
  • Radiation emitted by the furnace surface
  • Radiation emitted by the material
The net radiation is the difference between what the material receives and what it emits. Combine it with convection to find overall heat loss, which reflects real-world scenarios where surfaces are constantly interacting with their environments through multiple types of heat transfer.

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Most popular questions from this chapter

Solar radiation incident on the earth's surface may be divided into the direct and diffuse components described in Problem 12.9. Consider conditions for a day in which the intensity of the direct solar radiation is \(I_{\text {dir }}=210 \times 10^{7} \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{sr}\) in the solid angle subtended by the sun with respect to the earth, \(\Delta \omega_{s}=6.74 \times 10^{-5} \mathrm{sr}\). The intensity of the diffuse radiation is \(I_{\text {dif }}=70 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{sr}\). (a) What is the total solar irradiation at the earth's surface when the direct radiation is incident at \(\theta=30^{\circ}\) ? (b) Verify the prescribed value for \(\Delta \omega_{s}\), recognizing that the diameter of the sun is \(1.39 \times 10^{9} \mathrm{~m}\) and the distance between the sun and the earth is \(1.496 \times 10^{11} \mathrm{~m}\) (1 astronomical unit).

A thermocouple whose surface is diffuse and gray with an emissivity of \(0.6\) indicates a temperature of \(180^{\circ} \mathrm{C}\) when used to measure the temperature of a gas flowing through a large duct whose walls have an emissivity of \(0.85\) and a uniform temperature of \(450^{\circ} \mathrm{C}\). (a) If the convection heat transfer coefficient between the thermocouple and the gas stream is \(h=125 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and there are negligible conduction losses from the thermocouple, determine the temperature of the gas. (b) Consider a gas temperature of \(125^{\circ} \mathrm{C}\). Compute and plot the thermocouple measurement error as a function of the convection coefficient for \(10 \leq 5\) \(h \leq 1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). What are the implications of your results?

The energy flux associated with solar radiation incident on the outer surface of the earth's atmosphere has been accurately measured and is known to be \(1368 \mathrm{~W} / \mathrm{m}^{2}\). The diameters of the sun and earth are \(1.39 \times 10^{9}\) and \(1.27 \times 10^{7} \mathrm{~m}\), respectively, and the distance between the sun and the earth is \(1.5 \times 10^{11} \mathrm{~m}\). (a) What is the emissive power of the sun? (b) Approximating the sun's surface as black, what is its temperature? (c) At what wavelength is the spectral emissive power of the sun a maximum? (d) Assuming the earth's surface to be black and the sun to be the only source of energy for the earth, estimate the earth's surface temperature.

Assuming the earth's surface is black, estimate its temperature if the sun has an equivalent blackbody temperature of \(5800 \mathrm{~K}\). The diameters of the sun and earth are \(1.39 \times 10^{9}\) and \(1.27 \times 10^{\top} \mathrm{m}\), respectively, and the distance between the sun and earth is \(1.5 \times 10^{11} \mathrm{~m}\).

An opaque surface, \(2 \mathrm{~m} \times 2 \mathrm{~m}\), is maintained at \(400 \mathrm{~K}\) and is simultaneously exposed to solar irradiation with \(G_{S}=1200 \mathrm{~W} / \mathrm{m}^{2}\). The surface is diffuse and its spectral absorptivity is \(\alpha_{\lambda}=0,0.8,0\), and \(0.9\) for \(0 \leq \lambda \leq\) \(0.5 \mu \mathrm{m}, 0.5 \mu \mathrm{m}<\lambda \leq 1 \mu \mathrm{m}, 1 \mu \mathrm{m}<\lambda \leq 2 \mu \mathrm{m}\), and \(\lambda>2 \mu \mathrm{m}\), respectively. Determine the absorbed irradiation, emissive power, radiosity, and net radiation heat transfer from the surface.

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