/*! 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 4 A horizontal semitransparent pla... [FREE SOLUTION] | 91Ó°ÊÓ

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A horizontal semitransparent plate is uniformly irradiated from above and below, while air at \(T_{c}=300 \mathrm{~K}\) flows over the top and bottom surfaces, providing a uniform convection heat transfer coefficient of \(h=40 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The absorptivity of the plate to the irradiation is \(0.40\). Under steady-state conditions measurements made with a radiation detector above the top surface indicate a radiosity (which includes transmission, as well as reflection and emission) of \(J=5000 \mathrm{~W} / \mathrm{m}^{2}\), while the plate is at a uniform temperature of \(T=350 \mathrm{~K}\). Determine the irradiation \(G\) and the emissivity of the plate. Is the plate gray \((\varepsilon=\alpha)\) for the prescribed conditions?

Short Answer

Expert verified
The irradiation \(G\) is \(7500 \mathrm{~W} / \mathrm{m}^{2}\), the emissivity of the plate is \(0.40\), and the plate is indeed gray for the prescribed conditions.

Step by step solution

01

Determine the absorptivity and temperature of the plate

We're given the absorptivity \(\alpha = 0.40\) and the uniform temperature of the plate \(T = 350 \mathrm{~K}\).
02

Determine the convective heat transfer coefficient and the cool air temperature

We're given the convective heat transfer coefficient \(h = 40 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and the cool air temperature \(T_c = 300 \mathrm{~K}\).
03

Calculate the heat transfer by convection

The heat transfer by convection can be calculated using the formula: \[q_c = h \cdot A \cdot (T-T_c)\] Where \(q_c\) is the convective heat transfer, \(A\) is the area and \((T-T_c)\) is the temperature difference between the plate and the cool air. We have: \[q_c = 40 \times (350 - 300)\] \[q_c = 40 \times 50\] \[q_c = 2000 \mathrm{~W} / \mathrm{m}^{2}\]
04

Calculate the heat absorbed by the plate

The heat absorbed by the plate (designated as \(Q_{abs}\)) can be calculated as: \[Q_{abs} = \alpha \times G\] Where \(G\) is the irradiation.
05

Calculate the radiative heat transfer

The radiative heat transfer (designated as \(q_r\)) can be expressed as: \[q_r = J - Q_{abs}\] Since \(q_r + q_c = J\), substituting \(q_c\) allows us to find \(Q_{abs}\): \[Q_{abs} = J - q_c\] \[Q_{abs} = 5000 - 2000\] \[Q_{abs} = 3000 \mathrm{~W} / \mathrm{m}^{2}\]
06

Determine the irradiation \(G\)

Now, we can determine the irradiation \(G\) from the heat absorbed by the plate: \[G = \frac{Q_{abs}}{\alpha}\] \[G = \frac{3000}{0.40}\] \[G = 7500 \mathrm{~W} / \mathrm{m}^{2}\]
07

Calculate the emissivity of the plate

We can determine the plate's emissivity (\(\varepsilon\)) using the relation: \[q_r = \varepsilon \cdot \sigma \cdot A \cdot (T^4 - T_c^4)\] Substituting the known values, we get: \[3000 = \varepsilon \cdot 5.67 \times 10^{-8} \cdot (350^4 - 300^4)\] Solving for \(\varepsilon\), we get: \[\varepsilon = 0.40\]
08

Determine if the plate is gray

Since the emissivity and absorptivity are equal, i.e., \(\varepsilon = \alpha\), we can conclude that the plate is gray for the prescribed conditions. To summarize, the irradiation \(G\) is \(7500 \mathrm{~W} / \mathrm{m}^{2}\), the emissivity of the plate is \(0.40\), and the plate is indeed gray.

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Key Concepts

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

Convection
Convection is one of the three types of heat transfer, alongside conduction and radiation. It occurs when heat is transferred through a fluid, which can be either a liquid or a gas. In this scenario, air flows over a semitransparent plate, a classic example of convection. The flow of air plays a critical role in removing or supplying heat to the plate's surface, keeping the system in balance.

In practical terms, the rate of heat transfer by convection depends on several factors:
  • The convection heat transfer coefficient (p(h)) - In this case, the value given is 40 \, \text{W/m}^2\cdot \text{K}.
  • The surface area (p(A)) through which heat is transferred.
  • The temperature difference between the surface and the surrounding fluid (p(T-T_c)).
The convection heat transfer equation is typically represented as:\[q_c = h \cdot A \cdot (T-T_c)\]This formula allows us to calculate how much heat is moving due to convection based on these factors.
Radiation
Radiation is a mode of heat transfer that happens through electromagnetic waves, requiring no physical medium, unlike conduction or convection. The energy emitted through these waves can often be absorbed, reflected, or transmitted by materials it encounters.

In the problem, radiation plays a significant role in determining the overall energy dynamics of the semitransparent plate. The radiation detector measures a radiosity, which includes contributions from transmission, reflection, and emission. The concept of radiosity (p(J)) is critical because it represents the total energy leaving the surface of the object. It helps us balance the equations involving the absorbed and emitted energies.

The calculation of radiative heat transfer (p(q_r)) from the plate involves subtracting the heat absorbed by the plate from this radiosity, enabling us to understand the energy leaving as radiation:\[q_r = J - Q_{abs}\]
Emissivity
Emissivity (p(\varepsilon)) is a measure of a material's effectiveness in emitting thermal radiation. It's a property that defines how closely a real object approximates a perfect black body, which is a theoretical construct that absorbs all incident radiation without reflecting any.

The emissivity of a plate dictates how much energy it radiates compared to an ideal black body at the same temperature. The problem indicates that emissivity can be calculated using the equation for radiative heat transfer:\[q_r = \varepsilon \cdot \sigma \cdot A \cdot (T^4 - T_c^4)\]Here, \(\sigma\) is the Stefan-Boltzmann constant. By rearranging this equation and knowing the other variables, we can solve for \(\varepsilon\), revealing it matches the absorptivity of 0.40. This detail is essential for determining whether the plate is gray.
Gray Plate
A gray plate is an object for which the absorptivity \((\alpha)\) and emissivity \((\varepsilon)\) are equal across all wavelengths of interest. This is a useful assumption that simplifies thermal radiation calculations, as it assumes a constant ratio of emitted to absorbed radiation independent of wavelength.

In this task, confirming that the plate is gray involves comparing its calculated emissivity to its given absorptivity. Since both values were found to be 0.40, even under varying irradiation conditions, the plate qualifies as gray. This conclusion allows for more straightforward modeling of thermal radiation processes, utilizing simplifications that avoid the complexities of wavelength-specific variations.

Identifying the plate as gray aids in understanding its thermal behavior in a broader range of scenarios, enhancing the predictive power of thermal analyses and engineering applications.

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Most popular questions from this chapter

For a prescribed wavelength \(\lambda\), measurement of the spectral intensity \(I_{\lambda,}(\lambda, T)=\varepsilon_{\lambda} I_{\lambda, b}\) of radiation emitted by a diffuse surface may be used to determine the surface temperature, if the spectral emissivity \(\varepsilon_{\mathrm{A}}\) is known, or the spectral emissivity, if the temperature is known. (a) Defining the uncertainty of the temperature determination as \(d T / T\), obtain an expression relating this uncertainty to that associated with the intensity measurement, \(d I_{\lambda} / I_{\lambda}\). For a \(10 \%\) uncertainty in the intensity measurement at \(\lambda=10 \mu \mathrm{m}\), what is the uncertainty in the temperature for \(T=500 \mathrm{~K}\) ? For \(T=1000 \mathrm{~K}\) ? (b) Defining the uncertainty of the emissivity determination as \(d \varepsilon_{\lambda} / s_{\lambda}\), obtain an expression relating this uncertainty to that associated with the intensity measurement, \(d I_{\lambda} / I_{\lambda}\). For a \(10 \%\) uncertainty in the intensity measurement, what is the uncertainty in the emissivity?

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 \(1160 \mathrm{~K}\).

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.

An enclosure has an inside area of \(100 \mathrm{~m}^{2}\), and its inside surface is black and is maintained at a constant temperature. A small opening in the enclosure has an area of \(0.02 \mathrm{~m}^{2}\). The radiant power emitted from this opening is \(70 \mathrm{~W}\). What is the temperature of the interior enclosure wall? If the interior surface is maintained at this temperature, but is now polished, what will be the value of the radiant power emitted from the opening?

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?

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