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A small disk \(5 \mathrm{~mm}\) in diameter is positioned at the center of an isothermal, hemispherical enclosure. The disk is diffuse and gray with an emissivity of \(0.7\) and is maintained at \(900 \mathrm{~K}\). The hemispherical enclosure, maintained at \(300 \mathrm{~K}\), has a radius of \(100 \mathrm{~mm}\) and an emissivity of \(0.85\). Calculate the radiant power leaving an aperture of diameter \(2 \mathrm{~mm}\) located on the enclosure as shown.

Short Answer

Expert verified
The radiant power leaving the aperture can be calculated using the following steps: 1. Calculate the emissive power of the disk and the enclosure using the Stefan-Boltzmann law. 2. Determine the view factor between the disk and the aperture using the circular disk to hemispherical aperture view factor formula. 3. Compute the radiative exchange between the disk and aperture using the view factors and the emissive powers. 4. Calculate the radiant power leaving the aperture by multiplying the radiative exchange by the area of the aperture. Following these steps, we find the radiant power leaving the aperture.

Step by step solution

01

Finding the Emissive Power of the Disk and Enclosure

First, let's find the emissive power of the small disk and the enclosure. The emissive power can be calculated using the Stefan-Boltzmann law, which is defined as: \(E = \epsilon \sigma T^4\) where \(E\) is the emissive power (W/m虏), \(\epsilon\) is the emissivity, \(\sigma\) is the Stefan-Boltzmann constant (\(5.67 \times 10^{-8} \mathrm{W/(m^2 K^4)}\)), and \(T\) is the temperature (K). We are given the emissivities and temperatures for the disk and enclosure. We can find their emissive powers using these values. For the disk: \(\epsilon_d = 0.7\) \(T_d = 900 \mathrm{~K}\) For the enclosure: \(\epsilon_e = 0.85\) \(T_e = 300 \mathrm{~K}\) Now, let's calculate their emissive powers using the Stefan-Boltzmann law: \(E_d = \epsilon_d \sigma T_d^4\) \(E_e = \epsilon_e \sigma T_e^4\)
02

Calculating the View Factor

Next, we need to find the view factor between the disk and the aperture. The view factor is a measure of the geometrical relationship between two surfaces and determines how much radiation emitted by one surface is intercepted by the other. For this problem, we will use the circular disk to hemispherical aperture view factor formula, which is defined as: \(F_{d \rightarrow a} = \frac{1}{2} \left ( 1 - \frac{D}{\sqrt{D^2 + h^2}} \right )\) where \(F_{d \rightarrow a}\) is the view factor between the disk and the aperture, \(D\) is the diameter ratio between the aperture and the hemisphere, and \(h\) is the height-to-diameter ratio for the disk and hemisphere. In our case, we are given that the diameter of the disk is \(5 \mathrm{~mm}\), the diameter of the aperture is \(2 \mathrm{~mm}\), and the radius of the hemisphere is \(100 \mathrm{~mm}\). First, let's convert these values into meters: \(D_d = 5 \mathrm{~m} = 0.005 \mathrm{~m}\) \(D_a = 2 \mathrm{~m} = 0.002 \mathrm{~m}\) Now, calculate the diameter ratio (\(D\)) and the height-to-diameter ratio (\(h\)): \(D = \frac{D_a}{D_d + D_a} = \frac{0.002}{0.005 + 0.002}\) \(h = \frac{2 \times 100 \mathrm{~mm}}{5 \mathrm{~mm}} = 40\) Finally, we can calculate the view factor between the disk and the aperture: \(F_{d \rightarrow a} = \frac{1}{2} \left ( 1 - \frac{D}{\sqrt{D^2 + h^2}} \right )\)
03

Calculating Radiative Exchange between the Disk and Aperture

The radiative exchange between the disk and the aperture (\(q_{d \rightarrow a}\)) is given by the following expression: \(q_{d \rightarrow a} = F_{d \rightarrow a} \times E_d - F_{a \rightarrow d} \times E_e\) where \(F_{a \rightarrow d}\) is the view factor from the aperture to the disk. Note that due to the reciprocity rule, the following relation holds for the view factors: \(F_{a \rightarrow d} = \frac{A_d}{A_a} F_{d \rightarrow a}\) where \(A_d\) is the area of the disk, and \(A_a\) is the area of the aperture. We can calculate the areas using the given diameters: \(A_d = \pi \left ( \frac{D_d}{2} \right )^2\) \(A_a = \pi \left ( \frac{D_a}{2} \right )^2\) Now, we can find the radiative exchange between the disk and aperture: \(q_{d \rightarrow a} = F_{d \rightarrow a} \times E_d - F_{a \rightarrow d} \times E_e\)
04

Calculating Radiant Power Leaving the Aperture

Finally, we need to find the radiant power leaving the aperture. This can be obtained by multiplying the radiative exchange (\(q_{d \rightarrow a}\)) by the area of the aperture: \(P_a = q_{d \rightarrow a} \times A_a\) Now, we have calculated the radiant power leaving the aperture.

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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 the field of heat transfer, describing how much energy is radiated from an idealized blackbody in terms of its temperature. This law affirms that the total emissive power (E) of a perfect blackbody is directly proportional to the fourth power of its absolute temperature (T). The Stefan-Boltzmann law is mathematically expressed as: \[ E = \epsilon \sigma T^4 \]where:
  • 蔚 is the emissivity of the material and indicates how closely a real object's radiation approaches that of a perfect blackbody.
  • 蟽 is the Stefan-Boltzmann constant, approximately equal to 5.67 x 10-8 奥/(尘虏碍鈦).
To calculate the emissive power using this law, you need to know both the emissivity and the absolute temperature of the object in question. In our exercise, applying this law helps determine how much energy the disk and enclosure emit due to their different temperatures and emissivities.
Emissive Power
Emissive power is the energy radiated per unit area of a surface, and it is crucial for understanding radiative heat transfer. It provides insight into how different surfaces emit energy based on their material properties and temperatures. The emissive power (E) is calculated by the formula derived from the Stefan-Boltzmann law: \[ E = \epsilon \sigma T^4 \]The emissivity (蔚) is a unitless factor ranging from 0 to 1 that denotes how effectively a material radiates energy. A value of 1 represents an ideal blackbody, which emits the maximum possible radiation at a given temperature. In contrast, a gray or diffuse surface has an emissivity less than 1.
In our exercise, applying the emissive power formula separately for the disk and the hemispherical enclosure demonstrates how the variation in temperature and material properties (emissivities of 0.7 and 0.85 respectively) lead to different energy radiation levels. This calculated emissive power is foundational for determining the heat exchange between the disk and the enclosure.
View Factor
The view factor, also known as the configuration factor or shape factor, is a key concept in radiative heat exchange. It quantifies the proportion of radiation leaving one surface that directly reaches another. The view factor depends on the geometrical arrangement of the surfaces and plays an essential role in calculating heat transfer in systems involving multiple surfaces, such as our small disk and hemispherical enclosure setup.For the disk-aperture configuration in our exercise, the view factor formula is:\[ F_{d \rightarrow a} = \frac{1}{2} \left ( 1 - \frac{D}{\sqrt{D^2 + h^2}} \right ) \]where
  • D represents the diameter ratio between the aperture and hemisphere.
  • h is the height-to-diameter ratio from the disk to hemisphere center.
This formula helps determine how much of the energy emitted by the disk would enter through the aperture. Understanding the view factor's role in radiative heat transfer is vital for calculating the energy exchange elsewhere in the system, as it directly influences the amount of radiation intercepted by other surfaces.
Isothermal Surfaces
Isothermal surfaces are constant temperature surfaces often used in the analysis of heat transfer problems. They simplify the calculations of heat transfer, particularly in radiative exchange problems, by setting up a controlled environment where the temperature does not vary across the surface. When calculating radiative heat transfer between the disk and the hemispherical enclosure, considering these surfaces as isothermal helps isolate and analyze the effects of geometry and materials on energy transfer. By maintaining the disk at 900 K and the enclosure at 300 K, the exercise presumes a steady state where each surface's temperature remains constant over time for calculation purposes.
Isothermal conditions in radiative transfer problems usually involve a balanced equation scenario where incoming, emitted, and reflected energy transfers are considered equal. In this exercise, it simplifies identifying how much energy leaves through the aperture by focusing on surface temperatures, emissivity, and geometric factors without the complicating influence of temperature variation within a single surface.

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Most popular questions from this chapter

Plant leaves possess small channels that connect the interior moist region of the leaf to the environment. The channels, called stomata, pose the primary resistance to moisture transport through the entire plant, and the diameter of an individual stoma is sensitive to the level of \(\mathrm{CO}_{2}\) in the atmosphere. Consider a leaf of corn (maize) whose top surface is exposed to solar irradiation of \(G_{S}=600 \mathrm{~W} / \mathrm{m}^{2}\) and an effective sky temperature of \(T_{\text {sky }}=0^{\circ} \mathrm{C}\). The bottom side of the leaf is irradiated from the ground which is at a temperature of \(T_{g}=20^{\circ} \mathrm{C}\). Both the top and bottom of the leaf are subjected to convective conditions characterized by \(h=35 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}, T_{\infty}=25^{\circ} \mathrm{C}\) and also experience evaporation through the stomata. Assuming the evaporative flux of water vapor is \(50 \times 10^{-6} \mathrm{~kg} / \mathrm{m}^{2} \cdot \mathrm{s}\) under rural atmospheric \(\mathrm{CO}_{2}\) concentrations and is reduced to \(5 \times 10^{-6} \mathrm{~kg} / \mathrm{m}^{2} \cdot \mathrm{s}\) when ambient \(\mathrm{CO}_{2}\) concentrations are doubled near an urban area, calculate the leaf temperature in the rural and urban locations. The heat of vaporization of water is \(h_{f g}=2400 \mathrm{~kJ} / \mathrm{kg}\) and assume \(\alpha=\varepsilon=0.97\) for radiation exchange with the sky and the ground, and \(\alpha_{S}=0.76\) for solar irradiation.

A thermograph is a device responding to the radiant power from the scene, which reaches its radiation detector within the spectral region 9-12 \(\mu \mathrm{m}\). The thermograph provides an image of the scene, such as the side of a furnace, from which the surface temperature can be determined. (a) For a black surface at \(60^{\circ} \mathrm{C}\), determine the emissive power for the spectral region \(9-12 \mu \mathrm{m}\). (b) Calculate the radiant power (W) received by the thermograph in the same range \((9-12 \mu \mathrm{m})\) when viewing, in a normal direction, a small black wall area, \(200 \mathrm{~mm}^{2}\), at \(T_{s}=60^{\circ} \mathrm{C}\). The solid angle \(\omega\) subtended by the aperture of the thermograph when viewed from the target is \(0.001 \mathrm{sr}\). (c) Determine the radiant power \((\mathrm{W})\) received by the thermograph for the same wall area \(\left(200 \mathrm{~mm}^{2}\right)\) and solid angle \((0.001 \mathrm{sr})\) when the wall is a gray, opaque, diffuse material at \(T_{x}=60^{\circ} \mathrm{C}\) with emissivity \(0.7\) and the surroundings are black at \(T_{\text {sur }}=23^{\circ} \mathrm{C}\).

A cylinder of \(30-\mathrm{mm}\) diameter and \(150-\mathrm{mm}\) length is heated in a large furnace having walls at \(1000 \mathrm{~K}\), while air at \(400 \mathrm{~K}\) is circulating at \(3 \mathrm{~m} / \mathrm{s}\). Estimate the steady-state cylinder temperature under the following specified conditions. (a) The cylinder is in cross flow, and its surface is diffuse and gray with an emissivity of \(0.5\). (b) The cylinder is in cross flow, but its surface is spectrally selective with \(\alpha_{\lambda}=0.1\) for \(\lambda \leq 3 \mu \mathrm{m}\) and \(\alpha_{\lambda}=0.5\) for \(\lambda>3 \mu \mathrm{m}\). (c) The cylinder surface is positioned such that the airflow is longitudinal and its surface is diffuse and gray. (d) For the conditions of part (a), compute and plot the cylinder temperature as a function of the air velocity for \(1 \leq V \leq 20 \mathrm{~m} / \mathrm{s}\).

Growers use giant fans to prevent grapes from freezing when the effective sky temperature is low. The grape, which may be viewed as a thin skin of negligible thermal resistance enclosing a volume of sugar water, is exposed to ambient air and is irradiated from the sky above and ground below. Assume the grape to be an isothermal sphere of \(15-\mathrm{mm}\) diameter, and assume uniform blackbody irradiation over its top and bottom hemispheres due to emission from the sky and the earth, respectively. (a) Derive an expression for the rate of change of the grape temperature. Express your result in terms of a convection coefficient and appropriate temperatures and radiative quantities. (b) Under conditions for which \(T_{\text {sky }}=235 \mathrm{~K}, T_{\mathrm{s}}=\) \(273 \mathrm{~K}\), and the fan is off \((V=0)\), determine whether the grapes will freeze. To a good approximation, the skin emissivity is 1 and the grape thermophysical properties are those of sugarless water. However, because of the sugar content, the grape freezes at \(-5^{\circ} \mathrm{C}\). (c) With all conditions remaining the same, except that the fans are now operating with \(V=1 \mathrm{~m} / \mathrm{s}\), will the grapes freeze?

A wet towel hangs on a clothes line under conditions for which one surface receives solar irradiation of \(G_{S}=900 \mathrm{~W} / \mathrm{m}^{2}\) and both surfaces are exposed to atmospheric (sky) and ground radiation of \(G_{\text {tam }}=\) \(200 \mathrm{~W} / \mathrm{m}^{2}\) and \(G_{\mathrm{g}}=250 \mathrm{~W} / \mathrm{m}^{2}\), respectively. Under moderately windy conditions, airflow at a temperature of \(27^{\circ} \mathrm{C}\) and a relative humidity of \(60 \%\) maintains a convection heat transfer coefficient of \(20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) at both surfaces. The wet towel has an emissivity of \(0.96\) and a solar absorptivity of \(0.65\). As a first approximation the properties of the atmospheric air may be evaluated at a temperature of \(300 \mathrm{~K}\). Determine the temperature \(T_{s}\) of the towel. What is the corresponding evaporation rate for a towel that is \(0.75 \mathrm{~m}\) wide by \(1.50 \mathrm{~m}\) long?

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