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Consider a spherical reactor of \(5-\mathrm{cm}\) diameter operating at steady conditions with a temperature variation that can be expressed in the form of \(T(r)=a-b r^{2}\), where \(a=850^{\circ} \mathrm{C}\) and $b=5 \times 10^{5} \mathrm{~K} / \mathrm{m}^{2}\(. The reactor is made of material with \)c=200 \mathrm{~J} / \mathrm{kg} \cdot{ }^{\circ} \mathrm{C}, k=40 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=9000 \mathrm{~kg} / \mathrm{m}^{3}$. If the heat generation of the reactor is suddenly set to $9 \mathrm{MW} / \mathrm{m}^{3}$, determine the time rate of temperature change in the reactor. Is the heat generation of the reactor suddenly increased or decreased to $9 \mathrm{MW} / \mathrm{m}^{3}$ from its steady operating condition?

Short Answer

Expert verified
#Answer# The heat generation of the reactor was increased from its steady operating condition.

Step by step solution

01

Calculate the initial heat generation rate

Using the temperature variation equation, \(T(r) = a - b\cdot r^2\) and the material properties (\(c, k, \rho\)), we first calculate the heat generation rate at steady-state operating conditions. The heat conduction equation for a spherical reactor at steady-state is given by: $$ \frac{d}{dr}\left( r^2 \cdot k\cdot \frac{d T}{dr}\right) = \rho\cdot Q_{gen}, $$ where \(Q_{gen}\) is the heat generation rate. Find \(\frac{d T}{dr}\) from the given function \(T(r)\), and substitute it into the equation to find the heat generation rate. Differentiating \(T(r)\), $$ \frac{d T}{dr} = -2\cdot b\cdot r. $$ Now, substitute this into the heat conduction equation: $$ \frac{d}{dr}\left( r^2\cdot k\cdot (-2\cdot b\cdot r)\right) = \rho\cdot Q_{gen}. $$ Differentiating once again, $$ (-6\cdot k\cdot b)\cdot r^2 = \rho\cdot Q_{gen}. $$ Now, we have an equation for the heat generation rate, \(Q_{gen}\). Before finding the value of \(Q_{gen}\), let's derive the equation for the time rate of temperature change.
02

Derive the time rate of temperature change equation

We use the following unsteady heat conduction equation for a spherical reactor: $$ \frac{1}{\alpha}\cdot \frac{\partial T}{\partial t} = \frac{1}{r^2}\cdot \frac{\partial}{\partial r}\left( r^2\cdot \frac{\partial T}{\partial r}\right) + \frac{Q_{gen}}{c\cdot \rho}, $$ where \(\alpha = \frac{k}{c\cdot \rho}\) is the thermal diffusivity. We have already found the derivative of \(T(r)\), so now we will substitute the \(\frac{d T}{dr}\), \(\frac{Q_{gen}}{c\cdot \rho}\), and the value for \(\alpha\) into the equation: $$ \frac{1}{\alpha}\cdot \frac{\partial T}{\partial t} = \frac{1}{r^2}\cdot \frac{\partial}{\partial r}\left( r^2\cdot (-2\cdot b\cdot r)\right) + \frac{Q_{gen}}{c\cdot \rho}. $$ We have computed the expression inside the derivative in Step 1. Substituting it and the value for \(\alpha\) leads to: $$ \frac{c\cdot \rho}{k}\cdot \frac{\partial T}{\partial t} = \frac{(-6\cdot k\cdot b)\cdot r^2}{r^2} + Q_{gen}. $$
03

Determine whether heat generation has increased or decreased

From the calculation in Step 1, we know that at steady-state, the heat generation is given by: $$ (-6\cdot k\cdot b)\cdot r^2 = \rho\cdot Q_{gen, SS}. $$ Now, calculate the heat generation rate \(Q_{gen, SS}\) using the given parameters: $$ Q_{gen, SS} = \frac{(-6\cdot k\cdot b)}{\rho} = \frac{-6 \times 40 \times 5 \times 10^{5}}{9000} = -1.33 \times 10^7 \mathrm{~W}/\mathrm{m}^3 = -13.3 \ \mathrm{MW}/\mathrm{m}^3. $$ The initial heat generation rate is -13.3 MW/m³, and since the heat generation rate was suddenly set to 9 MW/m³, which is a higher value than -13.3 MW/m³, we can conclude that the heat generation of the reactor was increased from its steady operating condition.

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Most popular questions from this chapter

Consider a chilled-water pipe of length \(L\), inner radius \(r_{1}\), outer radius \(r_{2}\), and thermal conductivity \(k\). Water flows in the pipe at a temperature \(T_{f}\), and the heat transfer coefficient at the inner surface is \(h\). If the pipe is well insulated on the outer surface, \((a)\) express the differential equation and the boundary conditions for steady one-dimensional heat conduction through the pipe, and (b) obtain a relation for the variation of temperature in the pipe by solving the differential equation.

Consider a short cylinder of radius \(r_{o}\) and height \(H\) in which heat is generated at a constant rate of \(\dot{e}_{\mathrm{gen}}\). Heat is lost from the cylindrical surface at \(r=r_{o}\) by convection to the surrounding medium at temperature \(T_{\infty}\) with a heat transfer coefficient of \(h\). The bottom surface of the cylinder at \(z=0\) is insulated, while the top surface at \(z=H\) is subjected to uniform heat flux \(\dot{q}_{H}\). Assuming constant thermal conductivity and steady two-dimensional heat transfer, express the mathematical formulation (the differential equation and the boundary conditions) of this heat conduction problem. Do not solve.

Consider a large plane wall of thickness \(L=0.05 \mathrm{~m}\). The wall surface at \(x=0\) is insulated, while the surface at \(x=L\) is maintained at a temperature of \(30^{\circ} \mathrm{C}\). The thermal conductivity of the wall is \(k=30 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and heat is generated in the wall at a rate of $\dot{e}_{\mathrm{gen}}=\dot{e}_{0} \dot{e}^{-0.5 \mathrm{l} / \mathrm{W}} \mathrm{W} / \mathrm{m}^{3}$ where \(\dot{e}_{\mathrm{gen}}=8 \times 10^{6} \mathrm{~W} / \mathrm{m}^{3}\). Assuming steady one-dimensional heat transfer, \((a)\) express the differential equation and the boundary conditions for heat conduction through the wall, (b) obtain a relation for the variation of temperature in the wall by solving the differential equation, and (c) determine the temperature of the insulated surface of the wall.

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