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Consider a 20 -cm-thick concrete plane wall \((k=0.77\) $\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\( subjected to convection on both sides with \)T_{\infty 1}=27^{\circ} \mathrm{C}\( and \)h_{1}=5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( on the inside and \)T_{\infty 22}=8^{\circ} \mathrm{C}$ and \(\mathrm{h}_{2}=12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) on the outside. Assuming constant thermal conductivity with no heat generation and negligible radiation, (a) express the differential equation and the boundary conditions for steady one-dimensional heat conduction through the wall, \((b)\) obtain a relation for the variation of temperature in the wall by solving the differential equation, and \((c)\) evaluate the temperatures at the inner and outer surfaces of the wall.

Short Answer

Expert verified
(a) Express the differential equation and boundary conditions for steady one-dimensional heat conduction through the wall. The differential equation for steady one-dimensional heat conduction is: $$ \frac{d^2T}{dx^2} = 0 $$ The boundary conditions at the inner and outer surfaces of the wall are: $$ -k\frac{dT}{dx}\Bigg|_{x=0} = h_1(T_1 - T_{\infty 1}) $$ $$ k\frac{dT}{dx}\Bigg|_{x=L} = h_2(T_{\infty 2}-T_2) $$ (b) Obtain a relation for the temperature variation in the wall by solving the differential equation. The temperature variation in the wall is given by the linear function: $$ T(x) = Ax + B $$ where the constants A and B are: $$ A = \frac{h_1 T_{\infty 1} + h_2 T_{\infty 2}}{h_1 + h_2 + k L^{-1}(h_1 h_2)} $$ $$ B= \frac{k(h_1+h_2) T_{\infty 1} +h_1 h_2 L(T_{\infty 2}-T_{\infty 1})}{(h_1+h_2)(h_1 + h_2 + k L^{-1}(h_1 h_2))} $$ (c) Evaluate the temperatures at the inner and outer surfaces of the wall. The temperatures at the inner and outer surfaces of the wall are: $$ T_1 = T(0) = B = \frac{k(h_1+h_2) T_{\infty 1} +h_1 h_2 L(T_{\infty 2}-T_{\infty 1})}{(h_1+h_2)(h_1 + h_2 + k L^{-1}(h_1 h_2))} $$ $$ T_2 = T(L) = AL + B = \frac{h_2 T_{\infty 1} + h_1 T_{\infty 2}}{h_1 + h_2 + k L^{-1}(h_1 h_2)} $$

Step by step solution

01

Express the differential equation for steady one-dimensional heat conduction

In the absence of heat generation and with constant thermal conductivity, the differential equation for steady one-dimensional heat conduction through the wall is given by: $$ \frac{d^2T}{dx^2} = 0 $$ where \(T\) is the temperature and \(x\) is the distance along the wall.
02

Express the boundary conditions

The boundary conditions at the inner and outer surfaces of the wall can be expressed using Fourier's law of heat conduction and Newton's law of cooling for convection. At the inner surface, we have $$ -k\frac{dT}{dx}\Bigg|_{x=0} = h_1(T_1 - T_{\infty 1}) $$ At the outer surface, we have $$ k\frac{dT}{dx}\Bigg|_{x=L} = h_2(T_{\infty 2}-T_2) $$ where \(k\) is the thermal conductivity, \(T_1\) and \(T_2\) are temperatures at the inner and outer surfaces of the wall, \(L\) is the thickness of the wall, and \(h_1\) and \(h_2\) are the inside and outside convection coefficients, respectively.
03

Solve the differential equation

Given that the second derivative of temperature over distance is zero, the solution to this differential equation is a linear temperature profile. Thus, we can express the temperature as a linear function of distance \(x\): $$ T(x) = Ax + B $$ where \(A\) and \(B\) are constants to be determined using the boundary conditions.
04

Apply the boundary conditions

Using the boundary conditions in Step 2, we can write two equations to solve for the constants \(A\) and \(B\): At \(x = 0\), we have $$ -kA = h_1(B - T_{\infty 1}) $$ At \(x = L\), we have $$ kA = h_2(T_{\infty 2} - (AL + B)) $$ Solving these equations simultaneously, we get the values of \(A\) and \(B\) as: $$ A = \frac{h_1 T_{\infty 1} + h_2 T_{\infty 2}}{h_1 + h_2 + k L^{-1}(h_1 h_2)} $$ and $$ B= \frac{k(h_1+h_2) T_{\infty 1} +h_1 h_2 L(T_{\infty 2}-T_{\infty 1})}{(h_1+h_2)(h_1 + h_2 + k L^{-1}(h_1 h_2))} $$
05

Evaluate the temperatures at the inner and outer surfaces

We can now use the temperature expression from Step 3 and the constants from Step 4 to find the temperatures at the inner and outer surfaces: At \(x=0\) (inner surface): $$ T_1 = T(0) = B = \frac{k(h_1+h_2) T_{\infty 1} +h_1 h_2 L(T_{\infty 2}-T_{\infty 1})}{(h_1+h_2)(h_1 + h_2 + k L^{-1}(h_1 h_2))} $$ At \(x=L\) (outer surface): $$ T_2 = T(L) = AL + B = \frac{h_2 T_{\infty 1} + h_1 T_{\infty 2}}{h_1 + h_2 + k L^{-1}(h_1 h_2)} $$ Given the values from the problem statement, substitute them into the expressions above to evaluate the temperatures at the inner and outer surfaces.

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Most popular questions from this chapter

Consider a steam pipe of length \(L\), inner radius \(r_{1}\), outer radius \(r_{2}\), and constant thermal conductivity \(k\). Steam flows inside the pipe at an average temperature of \(T_{i}\) with a convection heat transfer coefficient of \(h_{i}\). The outer surface of the pipe is exposed to convection to the surrounding air at a temperature of \(T_{0}\) with a heat transfer coefficient of \(h_{\sigma}\). Assuming steady one-dimensional heat conduction through the pipe, \((a)\) express the differential equation and the boundary conditions for heat conduction through the pipe material, (b) obtain a relation for the variation of temperature in the pipe material by solving the differential equation, and (c) obtain a relation for the temperature of the outer surface of the pipe.

A metal spherical tank is filled with chemicals undergoing an exothermic reaction. The reaction provides a uniform heat flux on the inner surface of the tank. The tank has an inner diameter of \(5 \mathrm{~m}\), and its wall thickness is \(10 \mathrm{~mm}\). The tank wall has a variable thermal conductivity given as \(k(T)=k_{0}(1+\beta T)\), where $k_{0}=9.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \beta=0.0018 \mathrm{~K}^{-1}\(, and \)T$ is in \(\mathrm{K}\). The area surrounding the tank has an ambient temperature of \(15^{\circ} \mathrm{C}\), the tank's outer surface experiences convection heat transfer with a coefficient of \(80 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\). Determine the heat flux on the tank's inner surface if the inner surface temperature is \(120^{\circ} \mathrm{C}\).

The temperatures at the inner and outer surfaces of a \(15-\mathrm{cm}\)-thick plane wall are measured to be \(40^{\circ} \mathrm{C}\) and $28^{\circ} \mathrm{C}$, respectively. The expression for steady, one-dimensional variation of temperature in the wall is (a) \(T(x)=28 x+40\) (b) \(T(x)=-40 x+28\) (c) \(T(x)=40 x+28\) (d) \(T(x)=-80 x+40\) (e) \(T(x)=40 x-80\)

Consider the uniform heating of a plate in an environment at a constant temperature. Is it possible for part of the heat generated in the left half of the plate to leave the plate through the right surface? Explain.

In metal processing plants, workers often operate near hot metal surfaces. Exposed hot surfaces are hazards that can potentially cause thermal burns on human skin. Metallic surfaces above \(70^{\circ} \mathrm{C}\) are considered extremely hot. Damage to skin can occur instantaneously upon contact with metallic surfaces at that temperature. In a plant that processes metal plates, a plate is conveyed through a series of fans to cool its surface in an ambient temperature of \(30^{\circ} \mathrm{C}\). The plate is \(25 \mathrm{~mm}\) thick and has a thermal conductivity of $13.5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The temperature at the bottom surface of the plate is monitored by an infrared (IR) thermometer. Obtain an expression for the variation of temperature in the metal plate. The IR thermometer measures the bottom surface of the plate to be \(60^{\circ} \mathrm{C}\). Determine the minimum value of the convection heat transfer coefficient needed to keep the top surface below \(47^{\circ} \mathrm{C}\).

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