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Consider a \(1.5\)-m-high and \(0.6-\mathrm{m}\)-wide plate whose thickness is \(0.15 \mathrm{~m}\). One side of the plate is maintained at a constant temperature of \(500 \mathrm{~K}\) while the other side is maintained at \(350 \mathrm{~K}\). The thermal conductivity of the plate can be assumed to vary linearly in that temperature range as \(k(T)=\) \(k_{0}(1+\beta T)\) where \(k_{0}=18 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and \(\beta=8.7 \times 10^{-4} \mathrm{~K}^{-1}\). Disregarding the edge effects and assuming steady onedimensional heat transfer, determine the rate of heat conduction through the plate. Answer: \(22.2 \mathrm{~kW}\)

Short Answer

Expert verified
Answer: The rate of heat conduction through the plate is approximately \(22.2\,\mathrm{kW}\).

Step by step solution

01

Write down the given quantities and desired output

We know the following: - Plate height (h) = \(1.5\,\mathrm{m}\) - Plate width (w) = \(0.6\,\mathrm{m}\) - Plate thickness (t) = \(0.15\,\mathrm{m}\) - Temperature on one side of the plate: \(T_1=500\,\mathrm{K}\) - Temperature on the other side of the plate: \(T_2=350\,\mathrm{K}\) - Thermal conductivity expression: \(k(T)=k_0(1+\beta T)\), with \(k_0=18\,\frac{\mathrm{W}}{\mathrm{m}\cdot \mathrm{K}}\) and \(\beta=8.7\times 10^{-4}\,\mathrm{K}^{-1}\) We want to find: Rate of heat conduction (Q) in \(\mathrm{kW}\).
02

Determine the average thermal conductivity of the plate

To simplify the problem, let's calculate the average thermal conductivity of the plate \((\bar{k})\): $$ \bar{k}=\frac{k(T_1)+k(T_2)}{2} $$ Plug in the values for \(k(T_1)\) and \(k(T_2)\) using the expression for \(k(T)\): $$ \bar{k}=\frac{k_0(1+\beta T_1)+k_0(1+\beta T_2)}{2} $$
03

Calculate the average thermal conductivity

Now, use the given values of \(k_0\), \(\beta\), \(T_1\), and \(T_2\) to find \(\bar{k}\): $$ \bar{k}=\frac{18(1+8.7\times 10^{-4}\times 500)+18(1+8.7\times 10^{-4}\times 350)}{2} $$ Calculate: $$ \bar{k}\approx20.57\,\frac{\text{W}}{\text{m}\cdot\text{K}} $$
04

Apply Fourier's Law of heat conduction

Using Fourier's Law in one dimension: $$ Q = \frac{(\bar{k})(h)(w)\Delta T}{t} $$ Insert values: $$ Q = \frac{(20.57)(1.5)(0.6)(500-350)}{0.15} $$
05

Calculate the rate of heat conduction

Now, compute Q: $$ Q\approx22,\!212\,\mathrm{W} $$ Convert watts to kilowatts: $$ Q\approx22.2\,\mathrm{kW} $$ The rate of heat conduction through the plate is approximately \(22.2 \,\mathrm{kW}\).

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Thermal Conductivity
The concept of thermal conductivity is essential in understanding how heat moves through materials. It measures a material's ability to conduct heat. Imagine thermal conductivity as the ease with which heat travels through a material.

- Materials with high thermal conductivity - Example: Metals like copper and aluminum. - Allow heat to pass through quickly.
- Materials with low thermal conductivity - Example: Wood and plastic. - Tend to trap heat, slowing down its passage.

In this problem, the thermal conductivity of the plate is temperature-dependent, expressed as a function varying with temperature: \[k(T) = k_0 (1+\beta T)\] Where, \(k_0 = 18 \, \mathrm{W/m \, K}\) is the base thermal conductivity and \(\beta = 8.7 \times 10^{-4} \mathrm{\, K^{-1}}\) represents the rate of change of conductivity with temperature.
Fourier's Law
Named after the physicist Jean-Baptiste Joseph Fourier, Fourier's Law of heat conduction describes the flow of heat through a material. It states that the rate of heat transfer through a solid is directly proportional to the negative of the temperature gradient and the area through which the heat flows.

The mathematical representation in one dimension is:\[Q = -kA \frac{dT}{dx}\]Where:- \(Q\) is the rate of heat transfer.- \(k\) is the thermal conductivity.- \(A\) is the area through which heat is flowing.- \(\frac{dT}{dx}\) is the temperature gradient across the material.

This relationship helps us determine how much heat moves from a hot to a cold place in our given material. In the exercise, we've made use of Fourier's Law by substituting the average thermal conductivity and other attributes of the plate to find the rate of heat conduction.
Temperature Gradient
The temperature gradient is a measure of how temperature changes over a distance within a material. It's a pivotal factor in analyzing heat conduction because it essentially drives the flow of heat from warm to cold regions.
  • In formula form, it's expressed as \(\frac{dT}{dx}\).
  • A larger gradient means more rapid heat transfer.
  • If the gradient is zero, there's no heat flow.
In the exercise, the temperature difference between one side of the plate (500 K) and the other side (350 K) creates a gradient that leads to heat moving through the plate. Calculating this gradient allows us to implement it in Fourier's Law, determining the rate of heat transfer.
Steady-State Heat Transfer
Steady-state heat transfer is a scenario where the temperature of the material remains constant over time. There are no temperature changes occurring within the system as time progresses. This simplification allows us to assume that the amount of heat entering any section of an object is equal to the amount of heat leaving it.

Applying this concept: - In any slice of the plate, the heat transferred doesn't accumulate or deplete. - Ensures predictability and ease of calculations. - Assumes that all changes reach a point where everything remains unchanged over time.
In the given exercise, assuming steady-state conditions implies a constant flow of heat through the plate without any variation, making it easier to calculate the rate of heat conduction.

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Most popular questions from this chapter

A spherical shell, with thermal conductivity \(k\), has inner and outer radii of \(r_{1}\) and \(r_{2}\), respectively. The inner surface of the shell is subjected to a uniform heat flux of \(\dot{q}_{1}\), while the outer surface of the shell is exposed to convection heat transfer with a coefficient \(h\) and an ambient temperature \(T_{c \infty}\). Determine the variation of temperature in the shell wall and show that the outer surface temperature of the shell can be expressed as \(T\left(r_{2}\right)=\left(\dot{q}_{1} / h\right)\left(r_{1} / r_{2}\right)^{2}+T_{\infty \text { co }}\).

Consider a large plane wall of thickness \(L=0.8 \mathrm{ft}\) and thermal conductivity \(k=1.2 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\). The wall is covered with a material that has an emissivity of \(\varepsilon=0.80\) and a solar absorptivity of \(\alpha=0.60\). The inner surface of the wall is maintained at \(T_{1}=520 \mathrm{R}\) at all times, while the outer surface is exposed to solar radiation that is incident at a rate of \(\dot{q}_{\text {solar }}=300 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}\). The outer surface is also losing heat by radiation to deep space at \(0 \mathrm{~K}\). Determine the temperature of the outer surface of the wall and the rate of heat transfer through the wall when steady operating conditions are reached.

How is the order of a differential equation determined?

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 dropped into a large body of water at \(T_{\infty}\) where it is cooled by convection with an average convection heat transfer coefficient of \(h\). Assuming constant 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.

A large plane wall has a thickness \(L=50 \mathrm{~cm}\) and thermal conductivity \(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). On the left surface \((x=0)\), it is subjected to a uniform heat flux \(\dot{q}_{0}\) while the surface temperature \(T_{0}\) is constant. On the right surface, it experiences convection and radiation heat transfer while the surface temperature is \(T_{L}=225^{\circ} \mathrm{C}\) and the surrounding temperature is \(25^{\circ} \mathrm{C}\). The emissivity and the convection heat transfer coefficient on the right surface are \(0.7\) and \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), respectively. Show that the variation of temperature in the wall can be expressed as \(T(x)=\left(\dot{q}_{0} / k\right)(L-x)+T_{L}\), where \(\dot{q}_{0}=5130 \mathrm{~W} / \mathrm{m}^{2}\), and determine the temperature of the left surface of the wall at \(x=0\).

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