Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

Define the spectral emissivity of a medium of thickness \(L\) in terms of the spectral absorption coefficient.

Short Answer

Expert verified
Question: Define the spectral emissivity of a medium with a given thickness L in terms of its spectral absorption coefficient. Answer: The spectral emissivity of a medium with thickness L can be defined in terms of its spectral absorption coefficient using the equation: \(E(\lambda) = 1 - \exp{(-\alpha (\lambda) \cdot L)}\).

Step by step solution

01

Recalling the Beer-Lambert Law

The Beer-Lambert law describes the process of absorption of radiation as it passes through a medium. The law states that the absorbed fraction of radiation is proportional to the medium's thickness and the spectral absorption coefficient. The law can be represented by the equation: \(A(\lambda) = 1 - \exp{(-\alpha (\lambda) \cdot L)}\) Here: - \(A(\lambda)\) represents the spectral absorptance - \(\alpha (\lambda)\) represents the spectral absorption coefficient - \(L\) represents the thickness of the medium
02

Kirchhoff's Law of Radiation

Kirchhoff's law states that the emissivity of a material equals its absorptivity at a specific frequency or wavelength. In mathematical terms: \(E(\lambda) = A(\lambda)\) Here: - \(E(\lambda)\) represents the spectral emissivity - \(A(\lambda)\) represents the spectral absorptance
03

Defining Spectral Emissivity in Terms of the Spectral Absorption Coefficient

Using Kirchhoff's law and the Beer-Lambert law, we can determine the spectral emissivity \(E(\lambda)\) in terms of the spectral absorption coefficient \(\alpha(\lambda)\) and the thickness \(L\) of the medium as follows: \(E(\lambda) = 1 - \exp{(-\alpha (\lambda) \cdot L)}\) This equation defines the spectral emissivity of a medium with thickness \(L\) in terms of its spectral absorption coefficient.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

The surfaces of a two-surface enclosure exchange heat with one another by thermal radiation. Surface 1 has a temperature of \(400 \mathrm{~K}\), an area of \(0.2 \mathrm{~m}^{2}\), and a total emissivity of \(0.4\). Surface 2 is black, has a temperature of \(800 \mathrm{~K}\), and has area of \(0.3 \mathrm{~m}^{2}\). If the view factor \(F_{12}\) is \(0.3\), the rate of radiation heat transfer between the two surfaces is (a) \(340 \mathrm{~W}\) (b) \(560 \mathrm{~W}\) (c) \(780 \mathrm{~W}\) (d) \(900 \mathrm{~W}\) (e) \(1160 \mathrm{~W}\)

Consider a gray and opaque surface at \(0^{\circ} \mathrm{C}\) in an environment at \(25^{\circ} \mathrm{C}\). The surface has an emissivity of \(0.8\). If the radiation incident on the surface is \(240 \mathrm{~W} / \mathrm{m}^{2}\), the radiosity of the surface is (a) \(38 \mathrm{~W} / \mathrm{m}^{2}\) (b) \(132 \mathrm{~W} / \mathrm{m}^{2}\) (c) \(240 \mathrm{~W} / \mathrm{m}^{2}\) (d) \(300 \mathrm{~W} / \mathrm{m}^{2}\) (e) \(315 \mathrm{~W} / \mathrm{m}^{2}\)

A spherical tank, with an inner diameter of \(D_{1}=3 \mathrm{~m}\), is filled with a solution undergoing an exothermic reaction that heats the surface to a uniform temperature of \(120^{\circ} \mathrm{C}\). To prevent thermal burn hazards, the tank is enclosed by a concentric outer cover that provides an evacuated gap of \(5 \mathrm{~cm}\) in the enclosure. Both spherical surfaces have the same emissivity of \(0.5\), and the outer surface is exposed to natural convection with a heat transfer coefficient of $5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$ and radiation heat transfer with the surroundings at a temperature of \(30^{\circ} \mathrm{C}\). Determine whether or not the vacuumed gap is sufficient to keep the outer surface temperature below $45^{\circ} \mathrm{C}$ to prevent thermal burns. If not, propose a solution to keep the outer surface temperature below \(45^{\circ} \mathrm{C}\).

Two square plates, with the sides \(a\) and \(b\) (and \(b>a\) ), are coaxial and parallel to each other, as shown in Fig. P13-142, and they are separated by a center-to-center distance of \(L\). The radiation view factor from the smaller to the larger plate, \(F_{a b+}\) is given by $$ F_{a b}=\frac{1}{2 A}\left\\{\left[(B+A)^{2}+4\right]^{0.5}-\left[(B-A)^{2}+4\right]^{0.5}\right\\} $$ where, \(A=a / L\) and \(B=b / L\). (a) Calculate the view factors \(F_{a b}\) and \(F_{b a}\) for $a=20 \mathrm{~cm}\(, \)b=60 \mathrm{~cm}\(, and \)L=40 \mathrm{~cm}$. (b) Calculate the net rate of radiation heat exchange between the two plates described above if \(T_{a}=800^{\circ} \mathrm{C}\), $T_{b}=200^{\circ} \mathrm{C}, \varepsilon_{a}=0.8\(, and \)\varepsilon_{b}=0.4$. (c) A large, square plate (with the side $c=2.0 \mathrm{~m}, \varepsilon_{c}=0.1$, and negligible thickness) is inserted symmetrically between the two plates such that it is parallel to and equidistant from them. For the data given above, calculate the temperature of this third plate when steady operating conditions are established.

Cryogenic fluid flows inside a 10-mm-diameter metal tube. The metal tube is enclosed by a concentric polypropylene tube with a diameter of \(15 \mathrm{~mm}\). The minimum temperature limit for polypropylene tube is \(-18^{\circ} \mathrm{C}\), specified by the ASME Code for Process Piping (ASME B31.3-2014, Table B-1). The gap between the concentric tubes is a vacuum. The inner metal tube and the outer polypropylene tube have emissivity values of \(0.5\) and \(0.97\), respectively. The concentric tubes are placed in a vacuum environment, where the temperature of the surroundings is \(0^{\circ} \mathrm{C}\). Determine the lowest temperature that the inner metal tube can go without cooling the polypropylene tube below its minimum temperature limit of $-18^{\circ} \mathrm{C}$. Assume both tubes have thin walls.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free