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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?

Short Answer

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Analyze the spectral absorptance of the four given diffuse surfaces, denoted as \(A_1(\lambda)\), \(A_2(\lambda)\), \(A_3(\lambda)\), and \(A_4(\lambda)\). Compare the absorptance values at different wavelengths to determine if they remain constant. If the absorptance is relatively constant for a surface, then it may be approximated as a gray surface. Based on the analysis, identify which surfaces can be approximated as being gray and conclude your findings.

Step by step solution

01

Analyze the spectral characteristics of the four given surfaces.

Here, given that the surfaces are diffuse, we analyze the spectral absorptance. Analyze each surface and take note of its absorptance at different wavelengths. Surface 1: Let's denote this surface's absorptance as \(A_1(\lambda)\). Surface 2: Let's denote this surface's absorptance as \(A_2(\lambda)\). Surface 3: Let's denote this surface's absorptance as \(A_3(\lambda)\). Surface 4: Let's denote this surface's absorptance as \(A_4(\lambda)\).
02

Evaluate the gray surface approximation

A surface may only be approximated as a gray surface if its absorptance, \(A(\lambda)\), remains constant for all wavelengths, \(\lambda\). Compare the values of \(A_1(\lambda)\), \(A_2(\lambda)\), \(A_3(\lambda)\), and \(A_4(\lambda)\) at different wavelengths. Determine which, if any, of these surfaces have relatively constant absorptance values.
03

Identify the gray surfaces

Based on the analysis of constant absorptance in step 2, identify the surfaces that may be approximated as being gray. Conclude your findings after identifying the gray surfaces.

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Key Concepts

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

Spectral Absorptance
Spectral absorptance is a measure of how much radiation a surface absorbs across different wavelengths. It's important in determining the thermal behavior of materials when exposed to light, such as sunlight. A material's absorptance, denoted as \( A(\lambda) \), is a dimensionless quantity that varies between 0 and 1, where 0 means no absorption and 1 indicates complete absorption of the incident radiation at a specific wavelength \( \lambda \).

For example, a surface that absorbs all blue light would have an absorptance of 1 at the wavelengths corresponding to blue light, typically around 450 to 495 nm. A perfect mirror, which reflects all incident light, would have an absorptance of 0 at all visible wavelengths. In the exercise, students are asked to analyze the spectral absorptance of different surfaces to identify those that could be approximated as gray - meaning their absorptance doesn't change much across the spectrum.
Diffuse Surfaces
Diffuse surfaces are those that scatter incoming radiation equally in all directions. This uniform scattering leads to a matte, non-reflective appearance. In contrast, a glossy finish would indicate a specular surface that reflects light at the same angle as it arrives. When dealing with diffuse surfaces, their spectral response is particularly important because such surfaces do not direct radiation in a preferred direction, and they need to be understood in terms of how they interact with radiation incident from all directions.

Diffuse surfaces are critical in applications such as solar heating or photovoltaics, where an even response to incoming light from the sky dome is essential. For solar radiation exposure, materials with a diffuse finish are preferred as they are less sensitive to the direction of the incoming light, providing a more consistent behavior under varying sun angles.
Solar Radiation Exposure
Solar radiation exposure refers to the amount of sunlight incident on a surface. This exposure is critical for understanding energy absorption, reflection, and transmission by materials. Solar radiation consists of a broad spectrum of wavelengths including ultraviolet (UV), visible light, and infrared (IR) radiation. How a material responds to solar radiation—whether it heats up, reflects light, or allows light to pass through—is heavily influenced by its spectral absorptance.

Solar radiation is a key factor for evaluating the performance and efficiency of thermal management systems, solar panels, and building materials. Materials that absorb more sunlight (higher absorptance) will typically heat up more, which could be either a desired effect for thermal collectors or an undesired effect for materials that shouldn't overheat.
Wavelength Dependency
Wavelength dependency in the context of spectral absorptance refers to the variation in a material's absorptance with the wavelength of the incident light. A gray surface approximation suggests that there is little to no wavelength dependency, and absorptance remains nearly constant across the solar spectrum. However, most real-world materials show a significant wavelength dependency; they absorb different wavelengths of light to varying degrees.

Understanding wavelength dependency is crucial for designing and selecting materials for color-dependent applications or energy absorption purposes. For instance, greenhouse materials are designed to admit visible light for photosynthesis while blocking IR radiation to prevent excessive heating. In the problem from the textbook, looking for a gray surface—a surface with minimal wavelength dependency—is a simplifying step that can help simplify complex calculations involving light and thermal interactions.

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Most popular questions from this chapter

A radiation thermometer is a radiometer calibrated to indicate the temperature of a blackbody. A steel billet having a diffuse, gray surface of emissivity \(0.8\) is heated in a furnace whose walls are at \(1500 \mathrm{~K}\). Estimate the temperature of the billet when the radiation thermometer viewing the billet through a small hole in the furnace indicates \(1160 \mathrm{~K}\).

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.

One scheme for extending the operation of gas turbine blades to higher temperatures involves applying a ceramic coating to the surfaces of blades fabricated from a superalloy such as inconel. To assess the reliability of such coatings, an apparatus has been developed for testing samples under laboratory conditions. The sample is placed at the bottom of a large vacuum chamber whose walls are cryogenically cooled and which is equipped with a radiation detector at the top surface. The detector has a surface area of \(A_{d}=10^{-5} \mathrm{~m}^{2}\), is located at a distance of \(L_{\text {sl }}=1 \mathrm{~m}\) from the sample, and views radiation originating from a portion of the ceramic surface having an area of \(\Delta A_{c}=10^{-4} \mathrm{~m}^{2}\). An electric heater attached to the bottom of the sample dissipates a uniform heat flux, \(q_{b}^{\prime \prime}\), which is transferred upward through the sample. The bottom of the heater and sides of the sample are well insulated. Consider conditions for which a ceramic coating of thickness \(L_{c}=0.5 \mathrm{~mm}\) and thermal conductivity \(k_{c}=\) \(6 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) has been sprayed on a metal substrate of thickness \(L_{s}=8 \mathrm{~mm}\) and thermal conductivity \(k_{s}=\) \(25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The opaque surface of the ceramic may be approximated as diffuse and gray, with a total, hemispherical emissivity of \(\varepsilon_{c}=0.8\). (a) Consider steady-state conditions for which the bottom surface of the substrate is maintained at \(T_{1}=1500 \mathrm{~K}\), while the chamber walls (including the surface of the radiation detector) are maintained at \(T_{w}=90 \mathrm{~K}\). Assuming negligible thermal contact resistance at the ceramic- substrate interface, determine the ceramic top surface temperature \(T_{2}\) and the heat flux \(q_{b}^{\prime \prime}\). (b) For the prescribed conditions, what is the rate at which radiation emitted by the ceramic is intercepted by the detector?

A radiation detector having a sensitive area of \(A_{d}=\) \(4 \times 10^{-6} \mathrm{~m}^{2}\) is configured to receive radiation from a target area of diameter \(D_{\mathrm{r}}=40 \mathrm{~mm}\) when located a distance of \(L_{t}=1 \mathrm{~m}\) from the target. For the experimental apparatus shown in the sketch, we wish to determine the emitted radiation from a hot sample of diameter \(D_{s}=\) \(20 \mathrm{~mm}\). The temperature of the aluminum sample is \(T_{s}=700 \mathrm{~K}\) and its emissivity is \(\varepsilon_{s}=0.1\). A ring- shaped cold shield is provided to minimize the effect of radiation from outside the sample area, but within the target area. The sample and the shield are diffuse emitters. (a) Assuming the shield is black, at what temperature, \(T_{\text {sho }}\) should the shield be maintained so that its emitted radiation is \(1 \%\) of the total radiant power received by the detector? (b) Subject to the parametric constraint that radiation emitted from the cold shield is \(0.05,1\), or \(1.5 \%\) of the total radiation received by the detector, plot the required cold shield temperature, \(T_{\text {sh }}\), as a function of the sample emissivity for \(0.05 \leq \varepsilon_{x} \leq 0.35\).

Solar irradiation of \(1100 \mathrm{~W} / \mathrm{m}^{2}\) is incident on a large, flat, horizontal metal roof on a day when the wind blowing over the roof causes a convection heat transfer coefficient of \(25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The outside air temperature is \(27^{\circ} \mathrm{C}\), the metal surface absorptivity for incident solar radiation is \(0.60\), the metal surface emissivity is \(0.20\), and the roof is well insulated from below. (a) Estimate the roof temperature under steady-state conditions. (b) Explore the effect of changes in the absorptivity, emissivity, and convection coefficient on the steady-state temperature. 12.108 Neglecting the effects of radiation absorption, emission, and scattering within their atmospheres, calculate the average temperature of Earth, Venus, and Mars assuming diffuse, gray behavior. The average distance from the sun of each of the three planets, \(L_{s p}\), along with their measured average temperatures, \(\bar{T}_{p}\), are shown in the table below. Based upon a comparison of the calculated and measured average temperatures, which planet is most affected by radiation transfer in its atmosphere? \begin{tabular}{lcc} \hline Planet & \(L_{x-p}(\mathbf{m})\) & \(\bar{T}_{p}(\mathbf{K})\) \\ \hline Venus & \(1.08 \times 10^{11}\) & 735 \\ Earth & \(1.50 \times 10^{11}\) & 287 \\ Mars & \(2.30 \times 10^{11}\) & 227 \\ \hline \end{tabular}

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