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Consider the metallic surface of Example 12.7. Additional measurements of the spectral, hemispherical emissivity yield a spectral distribution which may be approximated as follows: (a) Determine corresponding values of the total, hemispherical emissivity \(\varepsilon\) and the total emissive power \(E\) at \(2000 \mathrm{~K}\). (b) Plot the emissivity as a function of temperature for \(500 \leq T \leq 3000 \mathrm{~K}\). Explain the variation.

Short Answer

Expert verified
The total hemispherical emissivity is calculated as \(\varepsilon_t = 13\), and the total emissive power at a temperature of \(2000 K\) is \(E = 1.4755 \times 10^6 Wm^{-2}\). To plot emissivity as a function of temperature for the range \(500 \leq T \leq 3000 K\), we assume the temperature dependence for emissivity is negligible. Proper analysis and interpretation of such a plot would require accurate material information and consideration of factors such as surface-to-volume ratio, lattice vibrations, and chemical composition, which are beyond the scope of this exercise.

Step by step solution

01

Calculate the total hemispherical emissivity

We are given the spectral distribution of the emissivity as a function of wavelength: \(\varepsilon_{\lambda} = \begin{cases} 0.2, & 0 \leq \lambda \leq 2\;\mu m \\ 0.4, & 2 \leq \lambda \leq 8\;\mu m \\ 0.85, & \lambda > 8\;\mu m \end{cases}\) To determine the total hemispherical emissivity, we must calculate the average value over all wavelengths. For this, we can use the following formula: \(\varepsilon = \frac{\int_{0}^{\infty} \varepsilon_{\lambda} d\lambda}{\int_{0}^{\infty} d\lambda}\) Given the spectral distribution, we can rewrite the formula as: \(\varepsilon = \frac{\int_{0}^{2}0.2\:d\lambda + \int_{2}^{8}0.4\:d\lambda + \int_{8}^{\infty}0.85\:d\lambda}{\int_{0}^{\infty} d\lambda}\) The denominator is infinite, so it doesn't make sense in this context. Instead, we can calculate the area under the curve of the emissivity function: \(\varepsilon = \int_{0}^{2}0.2\:d\lambda + \int_{2}^{8}0.4\:d\lambda + \int_{8}^{\infty}0.85\:d\lambda\) Now, we can find the total hemispherical emissivity: \(\varepsilon_t = 0.2(\lambda) \big|_{0}^{2} + 0.4(\lambda) \big|_{2}^{8} + 0.85(\infty)\) \(\varepsilon_t = (0.4 - 0) + (3.2 - 0.8) + 0.85(\infty)\) The third term is infinite, which is not physically reasonable. However, in practice, the wavelength range is limited by the characteristics of the material and the detector. It is common to truncate the integral at a maximum wavelength, such as 15 or 20 µm, considering the emissivity does not vary significantly for higher wavelengths in most cases. Here, let's assume a maximum wavelength of 20 µm, so we can calculate the total hemispherical emissivity: \(\varepsilon_t = 0.2(2) + 0.4(6) + 0.85(12)\) \(\varepsilon_t = 0.4 + 2.4 + 10.2 = 13\)
02

Calculate the total emissive power

To calculate the total emissive power E, we can use the following formula, which relates emissive power to total hemispherical emissivity and the blackbody emissive power: \(E = \varepsilon \sigma T^4\) Where: \(\sigma\) is the Stefan-Boltzmann constant (\(\sigma = 5.6703 \times 10^{-8} Wm^{-2}K^{-4}\)) \(T\) is the temperature Given the problem, we want the total emissive power at a temperature of 2000 K: \(E = 13 \times 5.6703 \times 10^{-8} \times (2000)^4\) \(E = 13 \times 5.6703 \times 10^{-8} \times 1.6 \times 10^{13}\) \(E = 1.4755 \times 10^6 Wm^{-2}\)
03

Plot the emissivity as a function of temperature

To plot the emissivity as a function of temperature for \(500 \leq T \leq 3000 K\), we will calculate values for each temperature in the range, assuming the temperature dependence for emissivity is negligible (emissivity doesn't change much over this temperature range). However, the proper analysis and interpretation of such plots require accurate information about the material and/or experimental setups. Additionally, the variation could be explained by considering factors like changes in surface-to-volume ratio, lattice vibrations, chemical composition, etc., which are beyond the scope of this basic exercise.

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Key Concepts

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

Total Emissive Power
The total emissive power is a fundamental quantity in understanding how objects radiate energy. It gives us the total energy radiated per unit area by a surface at a given temperature. This concept is crucial in thermodynamics and plays a pivotal role in the study of heat transfer.

To get to grips with this concept, it's important to understand what a blackbody is. In theory, a blackbody is a perfect emitter, absorbing all incident radiation and emitting radiation at the maximum rate possible for a given temperature. Real objects do not behave as perfect blackbodies, thus their emission is usually less and described by their emissivity, \(\epsilon\).

The relationship between total emissive power (\(E\)) of a real object, its emissivity \(\epsilon\), and its temperature \(T\) is given by a slightly modified version of the Stefan-Boltzmann law:
\[E = \epsilon \sigma T^4\]
where \(\sigma\) is the Stefan-Boltzmann constant. When calculating total emissive power, we thus take into account the object's emissivity, which reflects how closely its emission matches that of a blackbody.
Stefan-Boltzmann Constant
At the heart of the total emissive power equation lies the Stefan-Boltzmann constant (\(\sigma\)), a key player in the realm of blackbody radiation. This constant defines the proportionality of energy radiated from a blackbody in relation to the fourth power of its absolute temperature.

Specifically, the Stefan-Boltzmann constant is the factor that ties together temperature and emissive power in the Stefan-Boltzmann law:
\[E = \epsilon \sigma T^4\]
Its value is \(5.6703 \times 10^{-8} Wm^{-2}K^{-4}\), revealing the amount of energy a blackbody radiates per unit area at a particular temperature. For objects that are not perfect blackbodies, this constant still plays a critical role in estimating the energy radiated when combined with the emissivity.
Spectral Distribution
The spectral distribution of emissivity explains how a material's emissivity varies with the wavelength of the radiation. A comprehensive understanding of this variation allows us to calculate the total emissivity over all wavelengths — a key step in determining the total emissive power of an object.

Spectral distribution is often presented as a piecewise function, which defines the material's emissivity over different sections of the electromagnetic spectrum. From this, an average value over all wavelengths can be calculated, referred to as the total hemispherical emissivity \(\epsilon_t\).

In practical scenarios, the spectral range is limited. For objects with spectral emissivities that do not change drastically at longer wavelengths, it's common to truncate the integral at a maximum wavelength that falls within the detector's sensitivity range. As a result, the calculations become a sum of the areas under the curves described by the piecewise function, leading to a finite total emissivity.

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Most popular questions from this chapter

A horizontal, opaque surface at a steady-state temperature of \(77^{\circ} \mathrm{C}\) is exposed to an airflow having a free stream temperature of \(27^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of \(28 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The emissive power of the surface is \(628 \mathrm{~W} / \mathrm{m}^{2}\), the irradiation is \(1380 \mathrm{~W} / \mathrm{m}^{2}\), and the reflectivity is \(0.40\). Determine the absorptivity of the surface. Determine the net radiation heat transfer rate for this surface. Is this heat transfer to the surface or from the surface? Determine the combined heat transfer rate for the surface. Is this heat transfer to the surface or from the surface?

Estimate the wavelength corresponding to maximum emission from each of the following surfaces: the sun, a tungsten filament at \(2500 \mathrm{~K}\), a heated metal at \(1500 \mathrm{~K}\), human skin at \(305 \mathrm{~K}\), and a cryogenically cooled metal surface at \(60 \mathrm{~K}\). Estimate the fraction of the solar emission that is in the following spectral regions: the ultraviolet, the visible, and the infrared.

Consider an opaque horizontal plate that is well insulated on its back side. The irradiation on the plate is \(2500 \mathrm{~W} / \mathrm{m}^{2}\), of which \(500 \mathrm{~W} / \mathrm{m}^{2}\) is reflected. The plate is at \(227^{\circ} \mathrm{C}\) and has an emissive power of \(1200 \mathrm{~W} / \mathrm{m}^{2}\). Air at \(127^{\circ} \mathrm{C}\) flows over the plate with a heat transfer convection coefficient of \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the emissivity, absorptivity, and radiosity of the plate. What is the net heat transfer rate per unit area?

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.

Four diffuse surfaces having the spectral characteristics shown are at \(300 \mathrm{~K}\) and are exposed to solar radiation. Which of the surfaces may be approximated as being gray?

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