Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

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.

Short Answer

Expert verified
Answer: The highest temperature within the stainless steel plate is approximately \(50.981^{\circ}C\), and the lowest temperature is \(30^{\circ}C\).

Step by step solution

01

Write down the heat equation for the plate

The one-dimensional heat conduction equation with heat generation is given by: \(\frac{d}{dx}\left(k \frac{dT}{dx}\right) + \dot{q}_{gen} =0 \) Where \(x\) is the direction perpendicular to the plate, \(k\) is the thermal conductivity of the material, \(T\) is the temperature as a function of \(x\), and \(\dot{q}_{gen}\) is the heat generation rate per unit volume.
02

Apply boundary conditions

Since both sides of the plate are exposed to the same environment, we can assume the temperature distribution is symmetric across the plate. Due to this symmetry, we only need to analyze half of the plate (from \(x=0\) to \(x=L/2\), where \(L\) is the plate's thickness). The boundary conditions are: 1. At the center of the thickness, there is symmetry, so \(\frac{dT}{dx}(0) = 0\). 2. At \(x=L/2\), we have a convective boundary condition, and can use Newton's law of cooling: \(-k \frac{dT}{dx}(L/2) = h[T(L/2) - T_\infty]\), where \(h\) is the heat transfer coefficient, and \(T_\infty\) is the ambient temperature.
03

Solve the heat equation

Integrate the heat equation once, considering the first boundary condition: \(\int_{0}^x \frac{d}{dx'}(k \frac{dT}{dx'})dx' = -\int_{0}^x \dot{q}_{gen} dx'\) \(k \frac{dT}{dx} = -\dot{q}_{gen}x + C_1 \) Using the first boundary condition, we find \(C_1 = 0\): \(k \frac{dT}{dx}(0) = 0 \Rightarrow C_1 = 0\) Then the temperature distribution is given by: \(\frac{dT}{dx} = -\frac{\dot{q}_{gen}}{k}x \) Integrating this expression, we obtain the temperature distribution as a function of \(x\): \(T(x) = -\frac{\dot{q}_{gen}}{2k}x^2 + C_2\)
04

Solve for the integration constant C_2

To determine the integration constant \(C_2\), we use the second boundary condition: \(-k \frac{dT}{dx}(\frac{L}{2}) = h[T(\frac{L}{2}) - T_\infty]\) Substitute the temperature expression: \(-k\left(-\frac{\dot{q}_{gen}}{k}\frac{L}{2}\right) = h\left[-\frac{\dot{q}_{gen}}{2k}\left(\frac{L}{2}\right)^2 + C_2 - T_\infty\right]\) Solve for \(C_2\): \(C_2 = T_\infty - \frac{\dot{q}_{gen}L^2}{16k} + \frac{\dot{q}_{gen}L}{8h}\) Now, we have the complete temperature distribution within the plate: \(T(x) = -\frac{\dot{q}_{gen}}{2k}x^2 + T_\infty - \frac{\dot{q}_{gen}L^2}{16k} + \frac{\dot{q}_{gen}L}{8h}\)
05

Determine the highest and the lowest temperatures

The highest temperature occurs at the center of the plate, which is at \(x=0\): \(T_{max} = T(0) = T_\infty - \frac{\dot{q}_{gen}L^2}{16k} + \frac{\dot{q}_{gen}L}{8h}\) The lowest temperature occurs at the surface of the plate, which is at \(x=L/2\): \(T_{min} = T(\frac{L}{2}) = T_\infty\) Plug in the given values and calculate the highest and lowest temperatures: \(T_{max} = 30 - \frac{5\times10^5 \times (0.03)^2}{16\times 15.1} + \frac{5\times 10^5\times 0.03}{8\times 60} \approx 50.981 ^{\circ}C\) \(T_{min} = 30^{\circ}C\) Therefore, the highest temperature occurs at the center of the plate and is approximately \(50.981^{\circ}C\), while the lowest temperature occurs at the surface of the plate and is \(30^{\circ}C\).

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!

Key Concepts

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

Thermal Conductivity
Thermal conductivity is a property of materials that describes their ability to conduct heat. In this exercise, we consider a stainless steel plate with a thermal conductivity of \(15.1 \, \mathrm{W/m \cdot K}\). This value tells us how quickly or slowly the material can transfer heat across its surface.

Higher thermal conductivity means better heat conduction. Metals like stainless steel are known for decent thermal conductivity compared to insulators like wood or plastic, which have low values. The formula for thermal conductivity is often used in heat equations to find out how heat distributes in a material.

In our case, the heat conduction in the steel plate is affected by its thermal conductivity, influencing how temperature changes from one part of the plate to another. This property is essential in determining where the hottest and coolest points will be on the plate when heat is generated.
Heat Generation
Heat generation refers to the creation of heat due to internal sources within an object. In this problem, the stainless steel plate generates heat uniformly at a rate of \(5 \times 10^{5} \, \mathrm{W/m^3}\). This means that throughout every unit volume of the material, a substantial amount of heat energy is produced.

Understanding heat generation helps predict how internal temperatures change over time. The heat generated inside the plate adds to the heat flowing through it, which influences the overall temperature distribution.

This internal heat production must be considered along with thermal conductivity to figure out how heat spreads in the plate. The generated heat contributes to increasing temperatures towards the center of the plate, which is a crucial aspect in solving such problems.
Boundary Conditions
Boundary conditions are rules that provide constraints at the borders of a material's surface. They are essential in determining the behavior of heat flow within an object.

In this example, the boundary conditions are set by the plate's environment. Both sides of the plate are at \(30^{\circ}\mathrm{C}\), and a heat transfer coefficient of \(60 \, \mathrm{W/m^2 \cdot K}\) applies, which describes how easily heat passes between the plate and its surroundings.

There is symmetry at the center of the plate, simplifying the problem. At \(x=0\), there's no heat flux, while at the surface \(x=L/2\), Newton's law of cooling applies. These boundary conditions greatly aid in finding the temperature profile across the plate. They impact where and how heat convection and conduction occur.
Temperature Distribution
The temperature distribution is the variation of temperature within the material. Determining how heat spreads along the plate provides insight into the warmest and coldest areas.

Using the thermal conductivity, heat generation, and boundary conditions, the temperature distribution can be derived. In our scenario, the temperature equation is \( T(x) = -\frac{\dot{q}_{gen}}{2k}x^2 + T_\infty - \frac{\dot{q}_{gen}L^2}{16k} + \frac{\dot{q}_{gen}L}{8h}\), where each part contributes to shaping the temperature profile.

With this formula, we calculated that the highest temperature is at the center of the plate, occurring because of the symmetry and high internal heat generation. Meanwhile, the surface closest to the environment remains at the lowest temperature, primarily dictated by external boundary conditions. This distribution is crucial in understanding where to observe the extremes in temperature changes across the material.

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 cylindrical nuclear fuel rod of \(1 \mathrm{~cm}\) in diameter is encased in a concentric tube of \(2 \mathrm{~cm}\) in diameter, where cooling water flows through the annular region between the fuel rod \((k=30 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) and the concentric tube. Heat is generated uniformly in the rod at a rate of \(50 \mathrm{MW} / \mathrm{m}^{3}\). The convection heat transfer coefficient for the concentric tube surface is \(2000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). If the surface temperature of the concentric tube is \(40^{\circ} \mathrm{C}\), determine the average temperature of the cooling water. Can one use the given information to determine the surface temperature of the fuel rod? Explain.

Heat is generated uniformly at a rate of \(4.2 \times 10^{6} \mathrm{~W} / \mathrm{m}^{3}\) in a spherical ball \((k=45 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) of diameter \(24 \mathrm{~cm}\). The ball is exposed to iced-water at \(0^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(1200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the temperatures at the center and the surface of the ball.

Consider a large plane wall of thickness \(L=0.4 \mathrm{~m}\), thermal conductivity \(k=1.8 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and surface area \(A=\) \(30 \mathrm{~m}^{2}\). The left side of the wall is maintained at a constant temperature of \(T_{1}=90^{\circ} \mathrm{C}\) while the right side loses heat by convection to the surrounding air at \(T_{\infty}=25^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(h=24 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Assuming constant thermal conductivity and no heat generation in the wall, \((a)\) express the differential equation and the boundary conditions for steady one-dimensional heat conduction through the wall, \((b)\) obtain a relation for the variation of temperature in the wall by solving the differential equation, and \((c)\) evaluate the rate of heat transfer through the wall. Answer: (c) \(7389 \mathrm{~W}\)

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 \(\dot{e}_{\text {gen }}=\dot{e}_{0} e^{-0.5 x / L} \mathrm{~W} / \mathrm{m}^{3}\) where \(\dot{e}_{0}=8 \times 10^{6} \mathrm{~W} / \mathrm{m}^{3}\). 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.

The variation of temperature in a plane wall is determined to be \(T(x)=52 x+25\) where \(x\) is in \(\mathrm{m}\) and \(T\) is in \({ }^{\circ} \mathrm{C}\). If the temperature at one surface is \(38^{\circ} \mathrm{C}\), the thickness of the wall is (a) \(0.10 \mathrm{~m}\) (b) \(0.20 \mathrm{~m}\) (c) \(0.25 \mathrm{~m}\) (d) \(0.40 \mathrm{~m}\) (e) \(0.50 \mathrm{~m}\)

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