/*! 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 37 The steady-state temperature dis... [FREE SOLUTION] | 91Ó°ÊÓ

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The steady-state temperature distribution in a semitransparent material of thermal conductivity \(k\) and thickness \(L\) exposed to laser irradiation is of the form $$ T(x)=-\frac{A}{k a^{2}} e^{-a x}+B x+C $$ (a) Obtain expressions for the conduction heat fluxes at the front and rear surfaces. (b) Derive an expression for \(\dot{q}(x)\). (c) Derive an expression for the rate at which radiation is absorbed in the entire material, per unit surface area. Express your result in terms of the known constants for the temperature distribution, the thermal conductivity of the material, and its thickness. where \(A, a, B\), and \(C\) are known constants. For this situation, radiation absorption in the material is manifested by a distributed heat generation term, \(\dot{q}(x)\).

Short Answer

Expert verified
In summary, for the given steady-state temperature distribution in a semitransparent material: (a) The conduction heat fluxes at the front and rear surfaces are: \(q_{front} = -\frac{Aa}{a^2} + kB\) \(q_{rear} = -\frac{Aa}{a^2}e^{-aL} + kB\) (b) The heat generation term, \(\dot{q}(x)\), is given by: \(\dot{q}(x) = -Aa^2e^{-ax}\) (c) The rate at which radiation is absorbed in the entire material, per unit surface area, is given by: \(R = \frac{A(e^{-aL} - 1)}{La}\)

Step by step solution

01

Find conduction heat fluxes at the front and rear surfaces using Fourier's law

Fourier's law of heat conduction states that the heat flux (rate of heat transfer per unit area), \(q(x)\), is proportional to the negative gradient of the temperature, i.e., \(q(x) = -k \frac{dT}{dx}\). Given the temperature distribution function \(T(x) = -\frac{A}{ka^2} e^{-ax} + Bx + C\), We first need to find its derivative with respect to \(x\): \(\frac{dT}{dx} = \frac{A}{ka^2}(-a)e^{-ax} + B\) Now, we can find the conduction heat fluxes at the front and rear surfaces using Fourier's law: At the front surface (\(x=0\)), \(q_{front} = -k \frac{dT}{dx} \Big|_{x=0} = k\frac{A}{ka^2}(-a)e^{0} - kB = -\frac{Aa}{a^2} + kB\) At the rear surface (\(x=L\)), \(q_{rear} = -k \frac{dT}{dx} \Big|_{x=L} = k\frac{A}{ka^2}(-a)e^{-aL} - kB = -\frac{Aa}{a^2}e^{-aL} + kB\)
02

Apply the heat conduction equation to derive an expression for \(\dot{q}(x)\)

Since the temperature distribution has reached a steady-state, the heat conduction equation takes the form: \(\frac{d^2T}{dx^2} = -\frac{\dot{q}(x)}{k}\) We have the first derivative of \(T(x)\) from step 1: \(\frac{dT}{dx} = \frac{A}{ka^2}(-a)e^{-ax} + B\) Now, we need to find the second derivative of \(T(x)\): \(\frac{d^2T}{dx^2} = \frac{A}{ka^2}(a^2)e^{-ax}\) Plug this into the heat conduction equation: \(\frac{A}{ka^2}(a^2)e^{-ax} = -\frac{\dot{q}(x)}{k}\) Multiplying both sides by \(-ka^2\), we get: \(\dot{q}(x) = -Aa^2e^{-ax}\)
03

Derive the expression for the rate at which radiation is absorbed in the entire material, per unit surface area

To find the rate at which radiation is absorbed in the entire material, integrate the heat generation term, \(\dot{q}(x)\), over the thickness \(L\). The result should be divided by \(L\) to obtain the rate per unit surface area. \(R = \frac{1}{L}\int_0^L \dot{q}(x)\,dx = \frac{1}{L}\int_0^L (-Aa^2e^{-ax})\,dx\) Now, we perform the integration \(R = \frac{1}{L}\left[-\frac{A}{a}e^{-ax}\Big|_0^L\right] = \frac{1}{L}\left[-\frac{A}{a}(e^{-aL} - 1)\right]\) Finally, we adjust the form to obtain the answer: \(R = \frac{A(e^{-aL} - 1)}{La}\) So, the rate at which radiation is absorbed in the entire material, per unit surface area, is given by: \(R = \frac{A(e^{-aL} - 1)}{La}\)

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Key Concepts

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

Steady-State Temperature Distribution
Understanding steady-state temperature distribution is essential when analyzing heat transfer materials. This concept refers to a scenario where the temperature within a material does not change with time, even as heat might be continuously added to it. In the context of our example, where a semitransparent material is subjected to laser irradiation, the provided mathematical expression for temperature,
\( T(x) = -\frac{A}{k a^{2}} e^{-a x} + B x + C \),
represents the steady-state scenario. Here, the variables \( A, a, B, \) and \( C \) are constants that incorporate material properties and the conditions under which it's being heated.
To elaborate, \( A \) and \( a \) can be influenced by the intensity and penetration depth of the radiation, \( B \) could indicate a linear temperature gradient due to other external conditions, and \( C \) is an initial temperature offset. It's critical to recognize that in steady-state, even though energy is continually flowing through the material, there's no accumulation of energy within the material—the inflow and outflow balance each other perfectly, so the temperature distribution remains constant.
Conduction Heat Flux
Conduction heat flux is a core concept in the study of thermodynamics as it describes how heat is transported within a material. According to Fourier's law, the heat flux \( q(x) \) can be defined as the rate of heat transfer per unit area, which is proportional to the negative temperature gradient. In basic terms, heat moves from regions of high temperature to regions of low temperature.
For our exercise, to find this conduction heat flux, we examine the derivative of the temperature distribution with respect to position,\( x \). This derivative provides us with the gradient needed for Fourier’s law. At the material's front surface (\(x=0\)) and rear surface (\(x=L\)), we observe different heat flux values:
\( q_{front} = -k \frac{dT}{dx} \Big|_{x=0} \) and \( q_{rear} = -k \frac{dT}{dx} \Big|_{x=L} \).
As we can see from the exercise, the presence of exponential and linear terms in our temperature expression leads to the differences in heat flux at the front and rear, which is intuitive since the material's exposure to the heat source is likely not uniform.
Radiation Absorption
Radiation absorption is how material takes in energy from electromagnetic radiation, such as from a laser, as in our exercise. The absorbed energy is typically converted into internal energy, leading to an increase in temperature. In our example, the distributed heat generation term \( \dot{q}(x) \) represents the rate at which the radiation is absorbed as a function of position.
To find the total rate of radiation absorption across the entire material, we integrate the distributed heat generation rate over the material's thickness. Dividing by the thickness gives us an average rate of absorption per unit surface area, as shown by the solution
\( R = \frac{A(e^{-aL} - 1)}{La} \).
Understanding this absorption is crucial because the manner in which material absorbs radiation can significantly impact the efficiency of thermal systems and devices such as solar panels, lasers, and even cooking appliances. In the case of semitransparent materials, the balance between the amount of radiation absorbed, transmitted, and reflected is essential for applications that require controlled heating.

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Most popular questions from this chapter

A cylinder of radius \(r_{o}\), length \(L\), and thermal conductivity \(k\) is immersed in a fluid of convection coefficient \(h\) and unknown temperature \(T_{\infty}\). At a certain instant the temperature distribution in the cylinder is \(T(r)=a+b r^{2}\), where \(a\) and \(b\) are constants. Obtain expressions for the heat transfer rate at \(r_{o}\) and the fluid temperature.

A composite rod consists of two different materials, \(\mathrm{A}\) and \(\mathrm{B}\), each of length \(0.5 \mathrm{~L}\). The thermal conductivity of Material \(\mathrm{A}\) is half that of Material \(\mathrm{B}\), that is, \(k_{\mathrm{A}} / k_{\mathrm{B}}=0.5\). Sketch the steady-state temperature and heat flux distributions, \(T(x)\) and \(q_{x}^{\prime \prime}\), respectively. Assume constant properties and no internal heat generation in either material.

Consider a one-dimensional plane wall of thickness \(2 L\). The surface at \(x=-L\) is subjected to convective conditions characterized by \(T_{\infty, 1}, h_{1}\), while the surface at \(x=+L\) is subjected to conditions \(T_{\infty, 2}, h_{2}\). The initial temperature of the wall is \(T_{0}=\left(T_{\infty, 1}+T_{\infty, 2}\right) / 2\) where \(T_{\infty, 1}>T_{\infty, 2}\) (a) Write the differential equation, and identify the boundary and initial conditions that could be used to determine the temperature distribution \(T(x, t)\) as a function of position and time. (b) On \(T-x\) coordinates, sketch the temperature distributions for the initial condition, the steady-state condition, and for two intermediate times for the case \(h_{1}=h_{2}\). (c) On \(q_{x}^{\prime \prime}-t\) coordinates, sketch the heat flux \(q_{x}^{\prime \prime}(x, t)\) at the planes \(x=0,-L\), and \(+L\). (d) The value of \(h_{1}\) is now doubled with all other conditions being identical as in parts (a) through (c). On \(T-x\) coordinates drawn to the same scale as used in part (b), sketch the temperature distributions for the initial condition, the steady-state condition, and for two intermediate times. Compare the sketch to that of part (b). (e) Using the doubled value of \(h_{1}\), sketch the heat flux \(q_{x}^{\prime \prime}(x, t)\) at the planes \(x=0,-L\), and \(+L\) on the same plot you prepared for part (c). Compare the two responses.

Consider a small but known volume of metal that has a large thermal conductivity. (a) Since the thermal conductivity is large, spatial temperature gradients that develop within the metal in response to mild heating are small. Neglecting spatial temperature gradients, derive a differential equation that could be solved for the temperature of the metal versus time \(T(t)\) if the metal is subjected to a fixed surface heat rate \(q\) supplied by an electric heater. (b) A student proposes to identify the unknown metal by comparing measured and predicted thermal responses. Once a match is made, relevant thermophysical properties might be determined, and, in turn, the metal may be identified by comparison to published property data. Will this approach work? Consider aluminum, gold, and silver as the candidate metals.

A method for determining the thermal conductivity \(k\) and the specific heat \(c_{p}\) of a material is illustrated in the sketch. Initially the two identical samples of diameter \(D=60 \mathrm{~mm}\) and thickness \(L=10 \mathrm{~mm}\) and the thin heater are at a uniform temperature of \(T_{i}=23.00^{\circ} \mathrm{C}\), while surrounded by an insulating powder. Suddenly the heater is energized to provide a uniform heat flux \(q_{o}^{\prime \prime}\) on each of the sample interfaces, and the heat flux is maintained constant for a period of time, \(\Delta t_{o}\). A short time after sudden heating is initiated, the temperature at this interface \(T_{o}\) is related to the heat flux as $$ T_{o}(t)-T_{i}=2 q_{o}^{\prime \prime}\left(\frac{t}{\pi \rho c_{p} k}\right)^{1 / 2} $$ For a particular test run, the electrical heater dissipates \(15.0 \mathrm{~W}\) for a period of \(\Delta t_{o}=120 \mathrm{~s}\), and the temperature at the interface is \(T_{o}(30 \mathrm{~s})=24.57^{\circ} \mathrm{C}\) after \(30 \mathrm{~s}\) of heating. A long time after the heater is deenergized, \(t \geqslant \Delta t_{0}\), the samples reach the uniform temperature of \(T_{o}(\infty)=33.50^{\circ} \mathrm{C}\). The density of the sample materials, determined by measurement of volume and mass, is \(\rho=3965 \mathrm{~kg} / \mathrm{m}^{3}\). Determine the specific heat and thermal conductivity of the test material. By looking at values of the thermophysical properties in Table A.1 or A.2, identify the test sample material.

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