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A 1-m-long and \(0.1\)-m-thick steel plate of thermal conductivity $35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$ is well insulated on both sides, while the top surface is exposed to a uniform heat flux of $5500 \mathrm{~W} / \mathrm{m}^{2}$. The bottom surface is convectively cooled by a fluid at \(10^{\circ} \mathrm{C}\) having a convective heat transfer coefficient of $150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Assuming one-dimensional heat conduction in the lateral direction, find the temperature at the midpoint of the plate. Discretize the plate thickness into four equal parts.

Short Answer

Expert verified
Answer: The final step to find the temperature at the midpoint of the steel plate is to calculate the average between the temperatures at the second and third intermediate points, \(T_2\) and \(T_3\), as follows: \(T_{mid} =\dfrac{T_2 + T_3}{2}\).

Step by step solution

01

Set up the problem and choose discretization points

First, divide the thickness of the plate (0.1m) into four equal parts, leading to three intermediate points between the top and bottom surfaces. Let each discretization point be represented by \(T_i\) where \(i=1,2,3\). The temperature \(T_0\) is the temperature on the top surface and \(T_1\) is the first intermediate point's temperature, so on.
02

Write equations for each intermediate discretization point

For each intermediate point, apply the one-dimensional energy balance equation. The general equation for point \(i\) is: \(Q_{flux} + Q_{conv} = Q_{cond, i}\) (In this case, \(Q_{conv}\) is only present for \(i=1\) since the bottom surface is in contact with the fluid.) The equation can be developed as follows: \(i=1: 5500 + 150(T_1-10) = 35\dfrac{T_0 - T_1}{0.025}\) \(i=2: 5500 = 35\dfrac{T_1 - T_2}{0.025}\) \(i=3: 5500 = 35\dfrac{T_2 - T_3}{0.025}\)
03

Solve the system of equations

Solve the system of equations for the unknown \(T_1\), \(T_2\), and \(T_3\). You can use any method to solve the system of equations such as substitution or matrix inversion method.
04

Calculate temperature at the midpoint

Finally, to obtain the temperature at the midpoint, find the average between \(T_2\) and \(T_3\). Calculate the midpoint temperature \(T_{mid}\) as follows: \(T_{mid} =\dfrac{T_2 + T_3}{2}\)

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Most popular questions from this chapter

How does the finite difference formulation of a transient heat conduction problem differ from that of a steady heat conduction problem? What does the term \(\rho A \Delta x c_{p}\left(T_{m}^{i+1}-T_{m}^{i}\right) / \Delta t\) represent in the transient finite difference formulation?

What is the cause of the discretization error? How does the global discretization error differ from the local discretization error?

Is there any limitation on the size of the time step \(\Delta t\) in the solution of transient heat conduction problems using \((a)\) the explicit method and \((b)\) the implicit method?

Consider transient heat conduction in a plane wall with variable heat generation and constant thermal conductivity. The nodal network of the medium consists of nodes 0,1 , 2,3 , and 4 with a uniform nodal spacing of $\Delta x$. The wall is initially at a specified temperature. Using the energy balance approach, obtain the explicit finite difference formulation of the boundary nodes for the case of uniform heat flux \(\dot{q}_{0}\) at the left boundary (node 0 ) and convection at the right boundary (node 4) with a convection coefficient of \(h\) and an ambient temperature of \(T_{\infty}\). Do not simplify.

A hot brass plate is having its upper surface cooled by an impinging jet of air at a temperature of \(15^{\circ} \mathrm{C}\) and convection heat transfer coefficient of \(220 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The 10 -cm-thick brass plate $\left(\rho=8530 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=380 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k=110 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.\(, and \)\alpha=33.9 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}$ ) had a uniform initial temperature of \(650^{\circ} \mathrm{C}\), and the lower surface of the plate is insulated. Using a uniform nodal spacing of \(\Delta x=2.5 \mathrm{~cm}\) and time step of \(\Delta t=10 \mathrm{~s}\), determine \((a)\) the implicit finite difference equations and \((b)\) the nodal temperatures of the brass plate after 10 seconds of cooling.

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