/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 53 A two-layer wall is made of two ... [FREE SOLUTION] | 91Ó°ÊÓ

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A two-layer wall is made of two metal plates, with surface roughness of about \(25 \mu \mathrm{m}\), pressed together at an average pressure of \(10 \mathrm{MPa}\). The first layer is a stainless steel plate with a thickness of \(5 \mathrm{~mm}\) and a thermal conductivity of \(14 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The second layer is an aluminum plate with a thickness of \(15 \mathrm{~mm}\) and a thermal conductivity of \(237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). On the stainless steel side of the wall, the surface is subjected to a heat flux of \(800 \mathrm{~W} / \mathrm{m}^{2}\). On the aluminum side of the wall, the surface experiences convection heat transfer at an ambient temperature of \(20^{\circ} \mathrm{C}\), where the convection coefficient is \(12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the surface temperature of the stainless steel plate.

Short Answer

Expert verified
Based on the given information and the four-step solution, calculate the surface temperature of the stainless steel plate. Given: Thickness of Stainless Steel: 5 mm Thermal Conductivity of Stainless Steel: 14 W/m·K Thickness of Aluminum: 15 mm Thermal Conductivity of Aluminum: 237 W/m·K Heat Flux: 800 W/m² Convective Heat Transfer Coefficient: 12 W/m²·K Ambient Temperature: 20°C

Step by step solution

01

Calculate the resistance of each layer

Start by calculating the thermal resistance of each layer. This can be found using the equation: \(R = \dfrac{L}{k A}\) where \(R\) is the thermal resistance, \(L\) is the thickness of the layer, \(k\) is the thermal conductivity, and \(A\) is the surface area. In this case, we will assume the surface area is the same for both layers. The resistance of stainless steel, \(R_1\), and aluminum, \(R_2\), can be calculated as follows: \(R_1 = \dfrac{5 \times 10^{-3}~\mathrm{m}}{14~\mathrm{W/m \cdot K} A}\) \(R_2 = \dfrac{15 \times 10^{-3}~\mathrm{m}}{237~\mathrm{W/m \cdot K} A}\)
02

Calculate total resistance of the system

To find the total thermal resistance of the system, add the resistance of the stainless steel layer, the resistance of the aluminum layer, and the convective resistance: \(R_{total} = R_1 + R_2 + R_{conv}\) The convective resistance, \(R_{conv}\), can be calculated as: \(R_{conv} = \dfrac{1}{h A}\) where \(h\) is the convection heat transfer coefficient. Thus, we get: \(R_{conv} = \dfrac{1}{12~\mathrm{W/m^2 \cdot K} A}\) Now, we can calculate the total resistance: \(R_{total} = \dfrac{5 \times 10^{-3}~\mathrm{m}}{14~\mathrm{W/m \cdot K} A} + \dfrac{15 \times 10^{-3}~\mathrm{m}}{237~\mathrm{W/m \cdot K} A} + \dfrac{1}{12~\mathrm{W/m^2 \cdot K} A}\)
03

Determine the heat flux through the system

The heat flux, \(q\), through the system is given, which is \(800 \mathrm{~W} / \mathrm{m}^{2}\). To find the temperature difference between the surface of the stainless steel plate and the ambient temperature, we can use the following equation: \(\Delta T = q \times R_{total}\) Substitute \(q\) and \(R_{total}\) in the equation to get the temperature difference: \(\Delta T = 800~\mathrm{W/m^2} \left(\dfrac{5 \times 10^{-3}~\mathrm{m}}{14~\mathrm{W/m \cdot K} A} + \dfrac{15 \times 10^{-3}~\mathrm{m}}{237~\mathrm{W/m \cdot K} A} + \dfrac{1}{12~\mathrm{W/m^2 \cdot K} A}\right)\) Solve for \(\Delta T\): \(\Delta T = 9.52~\mathrm{K}\)
04

Determine the surface temperature of the stainless steel plate

Since we know the temperature difference \(\Delta T\) between the stainless steel surface and the aluminum surface and the ambient temperature is given as \(20^{\circ} \mathrm{C}\), we can find the surface temperature of the stainless steel plate. The heat flux through the wall is in the direction of aluminum to stainless steel plate, so to find the surface temperature of the stainless steel plate, we will subtract the temperature difference from the ambient temperature: \(T_{stainless~steel} = 20^{\circ} \mathrm{C} - 9.52~\mathrm{K}\) \(T_{stainless~steel} = 10.48^{\circ} \mathrm{C}\) Thus, the surface temperature of the stainless steel plate is \(10.48^{\circ} \mathrm{C}\).

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Key Concepts

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

Heat Transfer
Heat transfer is the movement of thermal energy from one part of an object to another or between objects. It occurs when there is a temperature difference. In this exercise, heat transfer takes place between the stainless steel and aluminum plates. The heat moves due to the temperature gradient, from the hotter region to the cooler one. Understanding the overall process of heat transfer helps us determine how effectively energy is being transferred and at what rate.
  • **Conduction:** The main form of heat transfer in solid objects like metals. It's driven by the thermal energy movement through material particles.
  • **Convection:** Involves the movement of heat by the physical movement of fluids. It's crucial when one of the surfaces interacts with a fluid.
  • **Radiation:** The energy transfer via electromagnetic waves, noticeable when significant temperature variations occur.
In our example of a two-layer wall, we particularly focus on conduction within the metal plates and convection when the heat crosses into the surrounding air.
Convection Coefficient
The convection coefficient, often denoted as 'h', is a crucial factor in determining heat transfer via convection. It tells us how efficiently heat is moved from a surface to a fluid or vice versa.
A higher convection coefficient implies quicker heat transfer, and its value is influenced by factors like:
  • **Fluid velocity**: Faster moving fluids enhance convective heat transfer.
  • **Fluid properties**: The density, viscosity, and thermal capacity play a role.
  • **Surface conditions**: Surface roughness and geometry can affect how easily a fluid can flow over the surface.
In our problem, the aluminum side of the wall has a convection coefficient of 12 W/m²·K, which suggests the level of heat transfer efficiency at the aluminum surface where it meets the surrounding air.
Thermal Conductivity
Thermal conductivity is a measure of a material's ability to conduct heat. In essence, it tells us how quickly heat can move through a material. Higher thermal conductivity indicates a better capacity of heat transfer through conduction.
This structural property changes with the material type, temperature, and the material's physical state.
  • **Metals**, like aluminum and stainless steel, generally have high thermal conductivities. Hence, they are good conductors.
  • **Material Specifics**: The exercise shows stainless steel with a thermal conductivity of 14 W/m·K and aluminum having a much higher thermal conductivity of 237 W/m·K.
    • These differences greatly influence the rate of heat transfer through each material, and thus, the final temperature at the interface and surface.
Heat Flux
Heat flux measures the rate of heat energy transfer per unit surface area. It's given in units such as W/m². In simple terms, it tells us how much thermal energy is flowing through a particular area.
Knowing the heat flux allows engineers and scientists to determine the temperature changes in materials over time.
  • **Magnitude and Direction**: It's given as positive or negative based on direction and indicates whether energy is entering or leaving a surface.
  • **Application**: In our scenario, a heat flux of 800 W/m² is applied to the stainless steel side, influencing the temperature distribution across the metal plates.
    • Calculating the resulting temperature informs us on the adequacy of insulation and material suitability for structural applications.

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Most popular questions from this chapter

The heat transfer surface area of a fin is equal to the sum of all surfaces of the fin exposed to the surrounding medium, including the surface area of the fin tip. Under what conditions can we neglect heat transfer from the fin tip?

Consider two identical people each generating \(60 \mathrm{~W}\) of metabolic heat steadily while doing sedentary work, and dissipating it by convection and perspiration. The first person is wearing clothes made of 1 -mm-thick leather \((k=\) \(0.159 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) ) that covers half of the body while the second one is wearing clothes made of 1 -mm-thick synthetic fabric \((k=0.13 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) that covers the body completely. The ambient air is at \(30^{\circ} \mathrm{C}\), the heat transfer coefficient at the outer surface is \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and the inner surface temperature of the clothes can be taken to be \(32^{\circ} \mathrm{C}\). Treating the body of each person as a 25 -cm-diameter, \(1.7-\mathrm{m}\)-long cylinder, determine the fractions of heat lost from each person by perspiration.

Steam at \(450^{\circ} \mathrm{F}\) is flowing through a steel pipe \(\left(k=8.7 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\right)\) whose inner and outer diameters are \(3.5\) in and \(4.0\) in, respectively, in an environment at \(55^{\circ} \mathrm{F}\). The pipe is insulated with 2 -in-thick fiberglass insulation \((k=\) \(\left.0.020 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\right)\). If the heat transfer coefficients on the inside and the outside of the pipe are 30 and \(5 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\), respectively, determine the rate of heat loss from the steam per foot length of the pipe. What is the error involved in neglecting the thermal resistance of the steel pipe in calculations?

The boiling temperature of nitrogen at atmospheric pressure at sea level ( 1 atm pressure) is \(-196^{\circ} \mathrm{C}\). Therefore, nitrogen is commonly used in low-temperature scientific studies since the temperature of liquid nitrogen in a tank open to the atmosphere will remain constant at \(-196^{\circ} \mathrm{C}\) until it is depleted. Any heat transfer to the tank will result in the evaporation of some liquid nitrogen, which has a heat of vaporization of \(198 \mathrm{~kJ} / \mathrm{kg}\) and a density of \(810 \mathrm{~kg} / \mathrm{m}^{3}\) at 1 atm. Consider a 3-m-diameter spherical tank that is initially filled with liquid nitrogen at 1 atm and \(-196^{\circ} \mathrm{C}\). The tank is exposed to ambient air at \(15^{\circ} \mathrm{C}\), with a combined convection and radiation heat transfer coefficient of \(35 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The temperature of the thin-shelled spherical tank is observed to be almost the same as the temperature of the nitrogen inside. Determine the rate of evaporation of the liquid nitrogen in the tank as a result of the heat transfer from the ambient air if the tank is \((a)\) not insulated, \((b)\) insulated with 5 -cm-thick fiberglass insulation \((k=0.035 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\), and (c) insulated with 2 -cm-thick superinsulation which has an effective thermal conductivity of \(0.00005 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

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