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Starting with an energy balance on a rectangular volume element, derive the one-dimensional transient heat conduction equation for a plane wall with constant thermal conductivity and no heat generation.

Short Answer

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Question: Derive the one-dimensional transient heat conduction equation for a plane wall with constant thermal conductivity and no heat generation. Answer: The one-dimensional transient heat conduction equation for a plane wall with constant thermal conductivity and no heat generation can be derived as: \(\frac{\partial T}{\partial t} = \frac{k}{\rho c_p} \frac{\partial^2 T}{\partial x^2}\) This equation shows how the temperature distribution within the plane wall changes with time due to heat conduction.

Step by step solution

01

Define the volume element

Let's define a rectangular volume element in the plane wall with width dx, height h, and length L. The volume of this element is V = h * L * dx.
02

Apply energy conservation principles

Perform an energy balance on the volume element. The rate at which energy enters the element minus the rate at which energy exits the element equals the rate at which energy is stored within the element.
03

Write energy balance equation

Let q(x) be the heat flux entering the element at x, and q(x+dx) be the heat flux leaving the element at x+dx. There is no heat generation within the element. Then, the energy balance equation can be written as: \(-q(x)A + q(x+dx)A = \frac{\partial}{\partial t}(V \rho c_p T)\) where A is the cross-sectional area of the element (h * L), ρ is the density, c_p is the specific heat, and T is the temperature.
04

Apply Fourier's Law

Since we are dealing with conduction heat transfer, we can apply Fourier's Law, which states that the heat flux is proportional to the temperature gradient and the thermal conductivity. For the plane wall with constant thermal conductivity k, we have: \(q(x) = -k \frac{\partial T}{\partial x}\) and \(q(x + dx) = -k \frac{\partial T(x+dx)}{\partial x}\)
05

Substitute Fourier's Law expressions into the energy balance equation

Now, substitute the Fourier's Law expressions from Step 4 into the energy balance equation from Step 3: \[kA \frac{\partial T}{\partial x} - kA \frac{\partial T(x+dx)}{\partial x} = hL \rho c_p \frac{\partial T}{\partial t} dx\]
06

Expand the Taylor series and simplify

Next, we expand the second term on the left side of the equation using Taylor's expansion: \(kA \frac{\partial T}{\partial x} - kA \left( \frac{\partial T}{\partial x} + \frac{\partial^2 T}{\partial x^2} dx \right) = hL \rho c_p \frac{\partial T}{\partial t} dx\) Simplify the equation by canceling terms and dividing by \(hL dx\): \(- k \frac{\partial^2 T}{\partial x^2} = \rho c_p \frac{\partial T}{\partial t}\)
07

Rearrange to get the one-dimensional heat conduction equation

Finally, we rearrange the equation to get the one-dimensional transient heat conduction equation for a plane wall with constant thermal conductivity and no heat generation: \(\frac{\partial T}{\partial t} = \frac{k}{\rho c_p} \frac{\partial^2 T}{\partial x^2}\) This is the desired equation, which shows how the temperature distribution within the plane wall changes with time due to heat conduction.

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Most popular questions from this chapter

The conduction equation boundary condition for an adiabatic surface with direction \(n\) being normal to the surface is (a) \(T=0\) (b) \(d T / d n=0\) (c) \(d^{2} T / d n^{2}=0\) (d) \(d^{3} T / d n^{3}=0\) (e) \(-k d T / d n=1\)

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?

Consider the base plate of an 800-W household iron with a thickness of $L=0.6 \mathrm{~cm}\(, base area of \)A=160 \mathrm{~cm}^{2}$, and thermal conductivity of \(k=20 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The inner surface of the base plate is subjected to uniform heat flux generated by the resistance heaters inside. When steady operating conditions are reached, the outer surface temperature of the plate is measured to be \(85^{\circ} \mathrm{C}\). Disregarding any heat loss through the upper part of the iron, \((a)\) express the differential equation and the boundary conditions for steady one- dimensional heat conduction through the plate, \((b)\) obtain a relation for the variation of temperature in the base plate by solving the differential equation, and \((c)\) evaluate the inner surface temperature. Answer: (c) \(100^{\circ} \mathrm{C}\)

Consider a large 3-cm-thick stainless steel plate $(k=15.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})$ in which heat is generated uniformly at a rate of \(5 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}\). Both sides of the plate are exposed to an environment at \(30^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(60 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Explain where in the plate the highest and the lowest temperatures will occur, and determine their values.

Consider uniform heat generation in a cylinder and in a sphere of equal radius made of the same material in the same environment. Which geometry will have a higher temperature at its center? Why?

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