/*! 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

Isothermal furnaces with small apertures approximating a blackbody are frequently used to calibrate heat flux gages, radiation thermometers, and other radiometric devices. In such applications, it is necessary to control power to the furnace such that the variation of temperature and the spectral intensity of the aperture are within desired limits. (a) By considering the Planck spectral distribution, Equation \(12.30\), show that the ratio of the fractional change in the spectral intensity to the fractional change in the temperature of the furnace has the form $$ \frac{d I_{\lambda} / I_{\lambda}}{d T / T}=\frac{C_{2}}{\lambda T} \frac{1}{1-\exp \left(-C_{2} / \lambda T\right)} $$ (b) Using this relation, determine the allowable variation in temperature of the furnace operating at \(2000 \mathrm{~K}\) to ensure that the spectral intensity at \(0.65 \mu \mathrm{m}\) will not vary by more than \(0.5 \%\). What is the allowable variation at \(10 \mu \mathrm{m}\) ?

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.

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).

The extremely high temperatures needed to trigger nuclear fusion are proposed to be generated by laserirradiating a spherical pellet of deuterium and tritium fuel of diameter \(D_{p}=1.8 \mathrm{~mm}\). (a) Determine the maximum fuel temperature that can be achieved by irradiating the pellet with 200 lasers, each producing a power of \(P=500 \mathrm{~W}\). The pellet has an absorptivity \(\alpha=0.3\) and emissivity \(\varepsilon=0.8\). (b) The pellet is placed inside a cylindrical enclosure. Two laser entrance holes are located at either end of the enclosure and have a diameter of \(D_{\mathrm{LEH}}=2 \mathrm{~mm}\). Determine the maximum temperature that can be generated within the enclosure.

Two plates, one with a black painted surface and the other with a special coating (chemically oxidized copper) are in earth orbit and are exposed to solar radiation. The solar rays make an angle of \(30^{\circ}\) with the normal to the plate. Estimate the equilibrium temperature of each plate assuming they are diffuse and that the solar flux is \(1368 \mathrm{~W} / \mathrm{m}^{2}\). The spectral absorptivity of the black painted surface can be approximated by \(\alpha_{\lambda}=0.95\) for \(0 \leq \lambda \leq \infty\) and that of the special coating by \(\alpha_{\lambda}=0.95\) for \(0 \leq \lambda<3 \mu \mathrm{m}\) and \(\alpha_{\lambda}=0.05\) for \(\lambda \geq 3 \mu \mathrm{m}\).

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