/*! 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 79 The air inside a chamber at \(T_... [FREE SOLUTION] | 91Ó°ÊÓ

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The air inside a chamber at \(T_{\infty, i}=50^{\circ} \mathrm{C}\) is heated convectively with \(h_{i}=20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) by a 200 -mm-thick wall having a thermal conductivity of \(4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and a uniform heat generation of \(1000 \mathrm{~W} / \mathrm{m}^{3}\). To prevent any heat generated within the wall from being lost to the outside of the chamber at \(T_{\infty, o}=25^{\circ} \mathrm{C}\) with \(h_{o}=5\) \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\), a very thin electrical strip heater is placed on the outer wall to provide a uniform heat flux, \(q_{\sigma^{\prime}}\) (a) Sketch the temperature distribution in the wall on \(T-x\) coordinates for the condition where no heat generated within the wall is lost to the outside of the chamber. (b) What are the temperatures at the wall boundaries, \(T(0)\) and \(T(L)\), for the conditions of part (a)? (c) Determine the value of \(q_{o}^{\prime \prime}\) that must be supplied by the strip heater so that all heat generated within the wall is transferred to the inside of the chamber. (d) If the heat generation in the wall were switched off while the heat flux to the strip heater remained constant, what would be the steady-state temperature, \(T(0)\), of the outer wall surface?

Short Answer

Expert verified
In summary, the temperature distribution in the wall is given by \(T(x) = T_{i} + \frac{h_{i}}{k}x\). The temperatures at the boundaries are \(T(0) = 50^{\circ}C\) and \(T(L) = 60^{\circ}C\). The heat flux supplied by the strip heater to prevent heat loss to the outside of the chamber is \(q_{o}'' = 0\frac{W}{m^2}\). When the heat generation in the wall is switched off, the steady-state temperature of the outer wall surface is \(T(0) = 25^{\circ}C\).

Step by step solution

01

Analyze the problem and define variables

: Let's start by defining the given parameters and variables: - \(T_{i} = 50^{\circ}C\): initial temperature inside the chamber - \(h_{i} = 20\frac{W}{m^{2}K}\): heat transfer coefficient from air to the wall - \(L = 0.2m\): thickness of the wall - \(k = 4\frac{W}{mK}\): thermal conductivity of the wall - \(Q_{gen} = 1000\frac{W}{m^{3}}\): uniform heat generation within the wall - \(T_{\infty, o} = 25^{\circ}C\): temperature outside of the chamber - \(h_{o} = 5\frac{W}{m^2K}\): heat transfer coefficient outside the chamber - \(q_{o}''\): heat flux supplied by the strip heater
02

Temperature distribution in the wall

: To find the temperature distribution in the wall, we need to first determine the heat transfer rate and then use the Fourier's law of conduction. The relation for the temperature distribution is: \[- k \frac{dT}{dx} = h_{i}(T-T_{i})\] Now, integrate the above equation to find the temperature distribution: \[T(x) = T_{i} + \frac{h_{i}}{k}x\]
03

Find Temperature at the wall boundaries \(T(0)\) and \(T(L)\)

: Now, plug in the boundary conditions to find the temperatures at the wall boundaries: a) At \(x=0\), \(T(0) = T_{i} = 50^{\circ}C\) b) At \(x=L\), \(T(L) = T_{i} + \frac{h_{i}}{k}L = 50 + \frac{20}{4}(0.2) = 50 + 10 = 60^{\circ}C\)
04

Find the heat flux supplied by the strip heater \(q_{o}''\)

: To find the value of \(q_{o}''\), we need to first determine the total heat generated in the wall and the heat transfer rate to the inside of the chamber: \[Q_{total} = Q_{gen}(L)A = 1000\times0.2A\] where \(A\) is the area of the wall. Now, the heat transfer rate to the inside of the chamber can be calculated as: \[Q_{transfer} = h_{i}A(T-T_{i}) = 20A(60-50) = 20A(10)\] To maintain the condition where no heat is lost to the outside of the chamber, the heat supplied by the strip heater should be equal to the difference between the total heat generated and the heat transferred to the inside of the chamber: \[q_{o}''A = Q_{total} - Q_{transfer} = 1000\times0.2A - 20A(10)\] Hence, \[q_{o}'' = 1000\times0.2 - 20(10) = 200 - 200 = 0\frac{W}{m^2}\]
05

Steady-state temperature of the outer wall surface \(T(0)\) when the heat generation is switched off

: In the case where the heat generation in the wall is switched off, the heat flux to the strip heater remains constant: \[0 = -k\frac{dT}{dx} + h_{o}(T_{\infty, o}-T)\] Now, let's rearrange the above equation to solve for the steady-state temperature: \[\frac{dT}{dx} = \frac{-h_{o}}{k}(T_{\infty, o}-T)\] Integrate the above equation to find the steady-state temperature: \[T(x) = T_{\infty, o} - \frac{h_{o}}{k}x\] At the outer wall surface \(x=0\), the steady-state temperature can be calculated as: \[T(0) = 25 - \frac{5}{4}(0) = 25^{\circ}C\] So, the steady-state temperature of the outer wall surface is \(25^{\circ}C\) when the heat generation in the wall is switched off.

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Key Concepts

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

Convective Heat Transfer
Heat transfer within a material, and between materials that are in direct contact, is conduction. On the other hand, convective heat transfer occurs when a fluid (gas or liquid) is involved, moving heat from one place to another. This process is governed by the convective heat transfer coefficient, denoted by 'h', measured in units of Watts per square meter Kelvin \(W/m^2K\).

For instance, in the textbook exercise, air inside a chamber transfers heat to the wall through convection with a given coefficient \( h_i \). This coefficient indicates how efficiently heat is being moved from the warm air to the wall's surface. The higher the value of 'h', the more efficient the process of heat transfer. If we place our hand over a heating vent, we can feel the convective heat transfer as warm air moves over our skin.

Understanding convective heat transfer is crucial, especially for designing heating and cooling systems, as it helps in predicting how quickly a space will reach a desired temperature. Additionally, this knowledge is vital to engineers who work on enhancing energy efficiency in buildings and industrial processes.
Thermal Conductivity
The rate at which heat passes through a material is determined by its thermal conductivity, denoted by 'k', with units of Watts per meter Kelvin \(W/mK\). This property quantifies how well a material can conduct heat. In the context of the exercise, the wall has a given thermal conductivity that allows heat to move from one side to the other.

The formula for heat conduction, based on Fourier’s law, is:\[ q = -k \frac{dT}{dx} \], where 'q' is the heat flux, \( \frac{dT}{dx} \) is the temperature gradient, and the negative sign indicates that heat flows from hot to cold regions.

When selecting materials for construction or manufacturing, knowing the thermal conductivity helps engineers ensure that components can handle the thermal loads they will encounter. High thermal conductivity materials are sought for heat sinks and other applications where efficient heat dissipation is crucial, while low thermal conductivity materials make great insulators.
Uniform Heat Generation
Sometimes, a material may generate heat evenly throughout its volume, a phenomenon described as uniform heat generation, denoted usually by \( Q_{gen} \) with the unit \( W/m^3 \). Electrical components like resistors, and mechanical processes such as friction in brakes, can cause uniform heat generation within a solid.

In our exercise, the wall has a specified uniform heat generation. This means that every unit volume of the wall generates the same amount of heat due to some internal mechanism. The presence of uniform heat generation significantly influences the temperature profile within the material, resulting in a non-linear temperature distribution, unless the material is perfectly insulated or in thermal equilibrium with its surroundings.

Managing uniform heat generation within materials is vital in electronic design, material processing, and in understanding geothermal gradients within the earth. Solutions to such problems require integrating concepts of both thermal conductivity and convective heat transfer to predict and control temperature distributions effectively.

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Most popular questions from this chapter

Consider the oven of Problem 1.54. The walls of the oven consist of \(L=30\)-mm- thick layers of insulation characterized by \(k_{\text {ins }}=0.03 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) that are sandwiched between two thin layers of sheet metal. The exterior surface of the oven is exposed to air at \(23^{\circ} \mathrm{C}\) with \(h_{\text {ext }}=2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The interior oven air temperature is \(180^{\circ} \mathrm{C}\). Neglecting radiation heat transfer, determine the steady-state heat flux through the oven walls when the convection mode is disabled and the free convection coefficient at the inner oven surface is \(h_{\mathrm{fr}}=3 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the heat flux through the oven walls when the convection mode is activated, in which case the forced convection coefficient at the inner oven surface is \(h_{\mathrm{fo}}=27 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Does operation of the oven in its convection mode result in significantly increased heat losses from the oven to the kitchen? Would your conclusion change if radiation were included in your analysis?

Two stainless steel plates \(10 \mathrm{~mm}\) thick are subjected to a contact pressure of 1 bar under vacuum conditions for which there is an overall temperature drop of \(100^{\circ} \mathrm{C}\) across the plates. What is the heat flux through the plates? What is the temperature drop across the contact plane?

In the design of buildings, energy conservation requirements dictate that the exterior surface area, \(A_{s}\), be minimized. This requirement implies that, for a desired floor space, there may be optimum values associated with the number of floors and horizontal dimensions of the building. Consider a design for which the total floor space, \(A_{f}\), and the vertical distance between floors, \(H_{f}\), are prescribed. (a) If the building has a square cross section of width \(W\) on a side, obtain an expression for the value of \(W\) that would minimize heat loss to the surroundings. Heat loss may be assumed to occur from the four vertical side walls and from a flat roof. Express your result in terms of \(A_{f}\) and \(H_{f}\) (b) If \(A_{f}=32,768 \mathrm{~m}^{2}\) and \(H_{f}=4 \mathrm{~m}\), for what values of \(W\) and \(N_{f}\) (the number of floors) is the heat loss minimized? If the average overall heat transfer coefficient is \(U=1 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and the difference between the inside and ambient air temperatures is \(25^{\circ} \mathrm{C}\), what is the corresponding heat loss? What is the percentage reduction in heat loss compared with a building for \(N_{f}=2\) ?

To maximize production and minimize pumping costs, crude oil is heated to reduce its viscosity during transportation from a production field. (a) Consider a pipe-in-pipe configuration consisting of concentric steel tubes with an intervening insulating material. The inner tube is used to transport warm crude oil through cold ocean water. The inner steel pipe \(\left(k_{s}=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\) has an inside diameter of \(D_{i, 1}=150 \mathrm{~mm}\) and wall thickness \(t_{i}=10 \mathrm{~mm}\) while the outer steel pipe has an inside diameter of \(D_{i, 2}=250 \mathrm{~mm}\) and wall thickness \(t_{o}=t_{i}\). Determine the maximum allowable crude oil temperature to ensure the polyurethane foam insulation \(\left(k_{p}=\right.\) \(0.075 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) between the two pipes does not exceed its maximum service temperature of \(T_{p, \max }=\) \(70^{\circ} \mathrm{C}\). The ocean water is at \(T_{\infty, o}=-5^{\circ} \mathrm{C}\) and provides an external convection heat transfer coefficient of \(h_{o}=500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The convection coefficient associated with the flowing crude oil is \(h_{i}=450 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (b) It is proposed to enhance the performance of the pipe-in-pipe device by replacing a thin \(\left(t_{a}=5 \mathrm{~mm}\right)\) section of polyurethane located at the outside of the inner pipe with an aerogel insulation material \(\left(k_{a}=0.012 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\). Determine the maximum allowable crude oil temperature to ensure maximum polyurethane temperatures are below \(T_{p, \max }=70^{\circ} \mathrm{C}\).

Rows of the thermoelectric modules of Example \(3.13\) are attached to the flat absorber plate of Problem 3.108. The rows of modules are separated by \(L_{\text {sep }}=0.5 \mathrm{~m}\) and the backs of the modules are cooled by water at a temperature of \(T_{w}=40^{\circ} \mathrm{C}\), with \(h=45 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the electric power produced by one row of thermoelectric modules connected in series electrically with a load resistance of \(60 \Omega\). Calculate the heat transfer rate to the flowing water. Assume rows of 20 immediately adjacent modules, with the lengths of both the module rows and water tubing to be \(L_{\text {row }}=20 W\) where \(W=54 \mathrm{~mm}\) is the module dimension taken from Example 3.13. Neglect thermal contact resistances and the temperature drop across the tube wall, and assume that the high thermal conductivity tube wall creates a uniform temperature around the tube perimeter. Because of the thermal resistance provided by the thermoelectric modules, it is no longer appropriate to assume that the temperature of the absorber plate directly above a tube is equal to that of the water.

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