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Consider a large 5 -cm-thick brass plate \((k=111\) $\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\( in which heat is generated uniformly at a rate of \)2 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$. One side of the plate is insulated, while the other side is exposed to an environment at \(25^{\circ} \mathrm{C}\) with a heat transfer coefficient of $44 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}$. Explain where in the plate the highest and the lowest temperatures will occur, and determine their values.

Short Answer

Expert verified
Answer: The highest temperature occurs at the insulated side of the plate and is equal to \(25^{\circ}C\), while the lowest temperature occurs at the exposed side of the plate, which can be calculated using the formula \(T(L) = \frac{kC_{1} - q'L^2}{hL} + T_{\infty}\).

Step by step solution

01

Convert Units

First, let's convert the thickness of the brass plate from cm to m: Thickness, \(L = \frac{5\,\text{cm}}{100} = 0.05\,\text{m}\)
02

Heat Transfer Differential Equation

The temperature distribution in the plate can be determined by the one-dimensional heat transfer equation with heat generation: $$ k\frac{d^2T}{dx^2} + q' = 0 $$ Here, we are given: Thermal conductivity, \(k = 111\) W/m.K Heat generation rate, \(q' = 2\times10^5\) W/m³
03

Integrate the Heat Transfer Equation Twice

First, we will integrate the heat transfer equation once to get: $$ \frac{dT}{dx} = -\frac{q'x}{k} + C_{1} $$ Then, we integrate it once more to find the temperature distribution: $$ T(x) = -\frac{q'x^2}{2k} + C_{1} x + C_{2} $$
04

Apply Boundary Conditions

For the insulated side (x=0), heat transfer is zero: $$ 0 = -h[T(0) - T_{\infty}] \Rightarrow T(0) = T_{\infty} = 25^{\circ}C $$ For the exposed side (x=L) with heat transfer coefficient h=44 W/m².K: $$ -k\frac{dT}{dx} |_{x=L} = -h[T(L) - T_{\infty}] $$
05

Determine Constants C1 and C2

Using the boundary conditions, we can determine the constants C1 and C2: From \(T(0) = T_{\infty}\), we get \(C_{2} = T_{\infty} = 25^{\circ}C\). Let's plug the boundary condition for x=L into the equation: $$ -k(\frac{-q'L}{k} + C_{1}) = -h[T(L) - T_{\infty}] $$ Solving for \(C_{1}\): $$ C_{1} = \frac{hL}{k}(T(L) - T_{\infty}) + q'L $$
06

Determine the Temperature Distribution

Substitute C1 and C2 back into the temperature equation: $$ T(x) = -\frac{q'x^2}{2k} + (\frac{hL}{k}(T(L) - T_{\infty}) + q'L) \cdot x + 25 $$
07

Identify the highest and the lowest temperature locations

Since the brass plate has one side insulated, the highest temperature occurs at this boundary (x=0) whereas the lowest temperature is exposed to the environment on the other boundary (x=L). Therefore, the highest temperature is \(T_{max}=T(0)=25^{\circ}C\), and the lowest temperature can be calculated at the exposed side (x=L).
08

Calculate the lowed temperature

To find \(T_{min}\), we need to calculate T(L) which we can get from the following relation from Step 5: $$ C_{1} = \frac{hL}{k}(T(L) - T_{\infty}) + q'L $$ Plug the known values and solve for \(T(L)\): $$ T(L) = \frac{kC_{1} - q'L^2}{hL} + T_{\infty} $$ Now, we can find \(T_{min}=T(L)\). Thus, the highest temperature occurs at the insulated side of the plate and is equal to \(25^{\circ}C\) while the lowest temperature occurs at the exposed side of the plate, which can be calculated using the formula above.

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Most popular questions from this chapter

Consider a function \(f(x)\) and its derivative \(d f / d x\). Does this derivative have to be a function of \(x\) ?

A large plane wall has a thickness \(L=50 \mathrm{~cm}\) and thermal conductivity \(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). On the left surface \((x=0)\), it is subjected to a uniform heat flux \(\dot{q}_{0}\) while the surface temperature \(T_{0}\) is constant. On the right surface, it experiences convection and radiation heat transfer while the surface temperature is \(T_{L}=225^{\circ} \mathrm{C}\) and the surrounding temperature is \(25^{\circ} \mathrm{C}\). The emissivity and the convection heat transfer coefficient on the right surface are \(0.7\) and $15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. (a) Show that the variation of temperature in the wall can be expressed as $T(x)=\left(\dot{q}_{0} / k\right)(L-x)+T_{L},(b)\( calculate the heat flux \)\dot{q}_{0}$ on the left face of the wall, and (c) determine the temperature of the left surface of the wall at \(x=0\).

Is the thermal conductivity of a medium, in general, constant or does it vary with temperature?

The variation of temperature in a plane wall is determined to be $T(x)=110 x-48 x\( where \)x\( is in \)\mathrm{m}\( and \)T\( is in \){ }^{\circ} \mathrm{C}$. If the thickness of the wall is \(0.75 \mathrm{~m}\), the temperature difference between the inner and outer surfaces of the wall is (a) \(110^{\circ} \mathrm{C}\) (b) \(74^{\circ} \mathrm{C}\) (c) \(55^{\circ} \mathrm{C}\) (d) \(36^{\circ} \mathrm{C}\) (e) \(18^{\circ} \mathrm{C}\)

A metal plate with a thickness of \(5 \mathrm{~cm}\) and a thermal conductivity of \(15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) has its bottom surface subjected to a uniform heat flux of \(2250 \mathrm{~W} / \mathrm{m}^{2}\). The upper surface of the plate is exposed to ambient air with a temperature of \(30^{\circ} \mathrm{C}\) and a convection heat transfer coefficient of $10 \mathrm{~W} / \mathrm{m}^{2}$. K. A series of ASME SA-193 carbon steel bolts are bolted onto the upper surface of a metal plate. The ASME Boiler and Pressure Vessel Code (ASME BPVC.IV-2015, HF-300) limits the maximum allowable use temperature to \(260^{\circ} \mathrm{C}\) for the \(\mathrm{SA}-193\) bolts. Formulate the temperature profile in the metal plate, and determine the location in the plate where the temperature begins to exceed $260^{\circ} \mathrm{C}\(. If the thread length of the bolts is \)1 \mathrm{~cm}$, would the \(\mathrm{SA}-193\) bolts comply with the ASME code?

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