A spherical metal ball of radius \(r_{o}\) is heated in an oven to a temperature of \(T_{i}\) throughout and is then taken out of the oven and allowed to cool in ambient air at \(T_{\infty}\) by convection and radiation. The emissivity of the outer surface of the cylinder is \(\varepsilon\), and the temperature of the surrounding surfaces is \(T_{\text {surr }}\). The average convection heat transfer coefficient is estimated to be \(h\). Assuming variable thermal conductivity and transient one-dimensional heat transfer, express the mathematical formulation (the differential equation and the boundary and initial conditions) of this heat conduction problem. Do not solve.

Short Answer

Expert verified
Question: Derive the mathematical formulation of the heat conduction problem for a spherical metal ball which is initially heated to a uniform temperature and then allowed to cool in ambient air, considering variable thermal conductivity and transient one-dimensional heat transfer. Answer: The mathematical formulation consists of the governing differential equation, initial condition, and boundary conditions. 1. Governing differential equation: \(\frac{\partial}{\partial r}\left(r^2 \alpha \frac{\partial T}{\partial r}\right) = r^2 \frac{\partial T}{\partial t}\) 2. Initial condition: \(T(r, 0) = T_i\) for \(0\le r\le r_o\) 3. Boundary conditions: \(\frac{\partial T}{\partial r}(0, t) = 0\) \(k\frac{\partial T}{\partial r}(r_o, t) = h(T(r_o, t) - T_\infty)+\varepsilon \sigma (T(r_o, t)^4 - T_{\text{surr}}^4)\)

Step by step solution

01

Write the general heat diffusion equation

The general heat diffusion equation for a variable thermal conductivity in spherical coordinates is given by: \(\frac{1}{r^2}\frac{\partial}{\partial r}\left(r^2 \alpha \frac{\partial T}{\partial r}\right)=\frac{\partial T}{\partial t}\) where \(\alpha\) is the thermal conductivity, \(T\) is the temperature, \(r\) is the radius, and \(t\) is the time.
02

Simplify the heat diffusion equation for one-dimensional heat transfer

For one-dimensional heat transfer (only radial direction), the equation provided in Step 1 simplifies to: \(\frac{\partial}{\partial r}\left(r^2 \alpha \frac{\partial T}{\partial r}\right) = r^2 \frac{\partial T}{\partial t}\) Now, we have the simplified heat diffusion equation for our problem. Next, we need to find the boundary and initial conditions for this problem.
03

Determine the initial condition

The initial condition is that the sphere is uniformly heated to a temperature of \(T_i\) throughout. Therefore, at the initial time \(t=0\), the temperature at any point within the sphere is given by: \(T(r, 0) = T_i\) for \(0\le r\le r_o\)
04

Determine the boundary conditions

We need to determine boundary conditions at the surface of the sphere \((r=r_o)\) and at the center \((r=0)\). Boundary condition at the center \((r=0)\): To maintain smoothness of the solution, the temperature gradient at the center should be zero. Therefore, \(\frac{\partial T}{\partial r}(0, t) = 0\) Boundary condition at the surface \((r=r_o)\): At the surface, convection and radiation take place. The heat flux due to convection and radiation can be given by: \(q_{conv} = h(T(r_o, t) - T_\infty)\) \(q_{rad} = \varepsilon \sigma (T(r_o, t)^4 - T_{\text{surr}}^4)\) The total heat flux at the surface is the sum of these two, and it is also equal to the heat conducted through the sphere. Hence, \(k\frac{\partial T}{\partial r}(r_o, t) = q_{conv} + q_{rad}\) Substituting the values for \(q_{conv}\) and \(q_{rad}\), \(k\frac{\partial T}{\partial r}(r_o, t) = h(T(r_o, t) - T_\infty)+\varepsilon \sigma (T(r_o, t)^4 - T_{\text{surr}}^4)\) Now, we have the boundary conditions for both ends. To summarize, 1. The differential equation governing the cooling process of the spherical ball: \(\frac{\partial}{\partial r}\left(r^2 \alpha \frac{\partial T}{\partial r}\right) = r^2 \frac{\partial T}{\partial t}\) 2. The initial condition: \(T(r, 0) = T_i\) for \(0\le r\le r_o\) 3. Boundary conditions: \(\frac{\partial T}{\partial r}(0, t) = 0\) \(k\frac{\partial T}{\partial r}(r_o, t) = h(T(r_o, t) - T_\infty)+\varepsilon \sigma (T(r_o, t)^4 - T_{\text{surr}}^4)\)

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

A spherical vessel is filled with chemicals undergoing an exothermic reaction. The reaction provides a uniform heat flux on the inner surface of the vessel. The inner diameter of the vessel is \(5 \mathrm{~m}\) and its inner surface temperature is at \(120^{\circ} \mathrm{C}\). The wall of the vessel has a variable thermal conductivity given as \(k(T)=k_{0}(1+\beta T)\), where \(k_{0}=1.01 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), \(\beta=0.0018 \mathrm{~K}^{-1}\), and \(T\) is in \(\mathrm{K}\). The vessel is situated in a surrounding with an ambient temperature of \(15^{\circ} \mathrm{C}\), the vessel's outer surface experiences convection heat transfer with a coefficient of \(80 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). To prevent thermal burn on skin tissues, the outer surface temperature of the vessel should be kept below \(50^{\circ} \mathrm{C}\). Determine the minimum wall thickness of the vessel so that the outer surface temperature is \(50^{\circ} \mathrm{C}\) or lower.

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.

A solar heat flux \(\dot{q}_{s}\) is incident on a sidewalk whose thermal conductivity is \(k\), solar absorptivity is \(\alpha_{s}\), and convective heat transfer coefficient is \(h\). Taking the positive \(x\) direction to be towards the sky and disregarding radiation exchange with the surroundings surfaces, the correct boundary condition for this sidewalk surface is (a) \(-k \frac{d T}{d x}=\alpha_{s} \dot{q}_{s}\) (b) \(-k \frac{d T}{d x}=h\left(T-T_{\infty}\right)\) (c) \(-k \frac{d T}{d x}=h\left(T-T_{\infty}\right)-\alpha_{s} \dot{q}_{s}\) (d) \(h\left(T-T_{\infty}\right)=\alpha_{s} \dot{q}_{s}\) (e) None of them

Exhaust gases from a manufacturing plant are being discharged through a 10 - \(\mathrm{m}\) tall exhaust stack with outer diameter of \(1 \mathrm{~m}\), wall thickness of \(10 \mathrm{~cm}\), and thermal conductivity of \(40 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The exhaust gases are discharged at a rate of \(1.2 \mathrm{~kg} / \mathrm{s}\), while temperature drop between inlet and exit of the exhaust stack is \(30^{\circ} \mathrm{C}\), and the constant pressure specific heat of the exhaust gasses is \(1600 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\). On a particular day, the outer surface of the exhaust stack experiences radiation with the surrounding at \(27^{\circ} \mathrm{C}\), and convection with the ambient air at \(27^{\circ} \mathrm{C}\) also, with an average convection heat transfer coefficient of \(8 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Solar radiation is incident on the exhaust stack outer surface at a rate of \(150 \mathrm{~W} / \mathrm{m}^{2}\), and both the emissivity and solar absorptivity of the outer surface are 0.9. Assuming steady one-dimensional heat transfer, (a) obtain the variation of temperature in the exhaust stack wall and (b) determine the inner surface temperature of the exhaust stack.

Consider a short cylinder of radius \(r_{o}\) and height \(H\) in which heat is generated at a constant rate of \(\dot{e}_{\text {gen. }}\). 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.

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