/*! 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 65 Common practice in chemical proc... [FREE SOLUTION] | 91Ó°ÊÓ

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Common practice in chemical processing plants is to clad pipe insulation with a durable, thick aluminum foil. The functions of the foil are to confine the batt insulation and to reduce heat transfer by radiation to the surroundings. Because of the presence of chlorine (at chlorine or seaside plants), the aluminum foil surface, which is initially bright, becomes etched with in- service time. Typically, the emissivity might change from \(0.12\) at installation to \(0.36\) with extended service. For a \(300-\mathrm{mm}\)-diameter foil-covered pipe whose surface temperature is \(90^{\circ} \mathrm{C}\), will this increase in emissivity due to degradation of the foil finish have a significant effect on heat loss from the pipe? Consider two cases with surroundings and ambient air at \(25^{\circ} \mathrm{C}\) : (a) quiescent air and (b) a cross-wind velocity of \(10 \mathrm{~m} / \mathrm{s}\).

Short Answer

Expert verified
For the quiescent air case (a), we have: - Initial radiation heat loss: \(q_{rad, initial} \approx 17.97 \ \text{W}\) - Degraded radiation heat loss: \(q_{rad, degraded} \approx 53.91 \ \text{W}\) - Convection heat loss: \(q_{conv} \approx 11.26 \ \text{W}\) The percentage change in total heat loss for case (a) is approximately 109%. For the 10 m/s cross-wind case (b), we have: - Initial radiation heat loss: \(q_{rad, initial} \approx 17.97 \ \text{W}\) - Degraded radiation heat loss: \(q_{rad, degraded} \approx 53.91 \ \text{W}\) - Convection heat loss: \(q_{conv} \approx 3934 \ \text{W}\) The percentage change in total heat loss for case (b) is approximately 1%. In conclusion, the increase in emissivity due to degradation of the foil finish has a significant effect on heat loss from the pipe in quiescent air conditions (case a), with a 109% increase. However, when a cross-wind of 10 m/s is present (case b), the effect of foil degradation on heat loss is minimal, with only a 1% increase.

Step by step solution

01

Calculate radiation heat loss

First, we'll calculate the radiation heat loss for the initial and degraded emissivity. The Stefan-Boltzmann law can be used for this calculation. The formula for radiation heat loss is: \[q_{rad} = \epsilon \sigma A (T_s^4 - T_a^4)\] where \(q_{rad}\) is the radiation heat loss, \(\epsilon\) is the emissivity, \(\sigma\) is the Stefan-Boltzmann constant (\(5.67 \times 10^{-8} \ \text{W}/\text{m}^{2}\text{K}^4\)), \(A\) is the surface area of the pipe, \(T_s\) is the surface temperature, and \(T_a\) is the ambient air temperature. Here, we have: - Initial emissivity: \(\epsilon_1 = 0.12\) - Degraded emissivity: \(\epsilon_2 = 0.36\) To determine the surface area of the pipe, we'll use the formula: \[A = 2 \pi R L\] where \(R\) is the radius of the pipe, and \(L\) is the length of the pipe. We are given the diameter, so to calculate the radius, we divide the diameter by 2: \[\text{Radius} = \frac{300 \ \text{mm}}{2} = 150 \ \text{mm} = 0.15 \ \text{m}\] Now, to keep things simple, let's assume a 1-meter length of the pipe (\(L = 1 \ \text{m}\)), since the percentage change in total heat loss would be the same for any length of the pipe. Thus, we have: \[A = 2 \pi (0.15 \ \text{m}) (1 \ \text{m}) = 0.942 \text{m}^2\] Now, we can calculate the radiation heat loss for both emissivities.
02

Calculate convection heat loss

Next, we will calculate the convection heat loss using the formula: \[q_{conv} = h A (T_s - T_a)\] where \(q_{conv}\) is the convection heat loss, \(h\) is the heat transfer coefficient in \(\text{W}/\text{m}^2\text{K}\), \(A\) is the surface area of the pipe, \(T_s\) is the surface temperature, and \(T_a\) is the ambient air temperature. For both cases (a) and (b), the thermal conductivity of air, \(k\), can be assumed constant at \(0.026 \ \text{W}/\text{mK}\). We need to find the heat transfer coefficient \(h\) for each case. (a) For the quiescent air case, we can use the formula for natural convection: \[h = \frac{k}{L}\text{Nu}\] \[h = \frac{0.026 \ \text{W}/\text{mK}}{0.15\text{m}} \times \text{Nu}\] Here, we'll utilize the Nusselt number, Nu, for natural convection. Using typical values for natural convection from vertical cylinders (Nu ≈ 1), we have: \[h = \frac{0.026 \ \text{W}/\text{mK}}{0.15\text{m}} \times 1 \approx 0.173 \ \text{W}/\text{m}^2\text{K}\] (b) For the 10 m/s cross-wind case, we can use the forced convection Dittus-Boelter correlation to find the Nusselt number: \[Nu = 0.023 \text{Re}^{0.8} \text{Pr}^{0.4} \pclose ^{*}\] where Re is the Reynolds number, Pr is the Prandtl number of air. We'll assume Pr to be a constant value of 0.71 for air. The Reynolds number can be determined using the formula: \[\text{Re} = \frac{\rho VD}{\mu}\] where \(\rho\) is the air density, \(V\) is the cross-wind velocity, \(D\) is the diameter, and \(\mu\) is the dynamic viscosity of air. Assuming standard atmospheric conditions, we have \(\rho = 1.184 \ \text{kg}/\text{m}^3\), and \(\mu = 1.847 \times 10^{-5} \ \text{kg}/\text{m}\text{s}\). From this, the Reynolds number can be determined: \[\text{Re} = \frac{(1.184 \ \text{kg}/\text{m}^3)(10 \ \text{m}/\text{s})(0.3 \ \text{m})}{1.847 \times 10^{-5} \ \text{kg}/\text{m}\text{s}} \approx 1.9 × 10^5\] Now, we can determine the Nusselt number: \[Nu \approx 0.023 \times (1.9 \times 10^5)^{0.8} \times 0.71^{0.4} \approx 350\] Finally, we can calculate the heat transfer coefficient for this case: \[h = \frac{0.026 \ \text{W}/\text{mK}}{0.15\text{m}} \times 350 \approx 60.33 \ \text{W}/\text{m}^2\text{K}\] Now we can calculate the convection heat loss for both cases.
03

Calculate the total heat loss and percentage change for each case

With the radiation and convection heat losses calculated, we can now calculate the total heat loss for each case and compare the percentage change between the initial and degraded emissivity. \[q_{total} = q_{rad} + q_{conv}\] Calculate this for both cases (a) and (b) with the initial and degraded emissivity. To evaluate the significance of the increase in emissivity, calculate the percentage change in total heat loss for each case. \[\% \text{ change} = \frac{q_{total, degraded} - q_{total, initial}}{q_{total, initial}} \times 100\] Compare the percentage change for the quiescent air case and the 10 m/s cross-wind case. This will provide insight into whether the degradation of the foil finish has a significant effect on heat loss from the pipe for these two scenarios.

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Key Concepts

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

Radiation Heat Transfer
Radiation heat transfer plays a crucial role in the energy exchange between surfaces and their environment. It involves the emission of electromagnetic waves caused by the thermal motion of charged particles within materials. Unlike convection and conduction, radiation does not require a medium to transfer heat, allowing energy to be exchanged even through a vacuum.

For insulated pipes, particularly those used in chemical processing plants, the surface's emissivity—a measure of a material's ability to emit thermal radiation—is an essential factor in determining how much heat is lost through radiation. In the exercise, the Stefan-Boltzmann law, given by the equation \(q_{rad} = \epsilon \sigma A (T_s^4 - T_a^4)\), is used to calculate this heat loss. Here, \(\sigma\) represents the Stefan-Boltzmann constant, and the temperatures \(T_s\) and \(T_a\) denote the surface and ambient air temperatures, respectively.

In the context of the problem, the foil's emissivity changes due to environmental exposure, directly influencing the radiation heat transfer rate. The emissivity increase from 0.12 to 0.36 is significant because radiation heat transfer is directly proportional to emissivity. Therefore, any changes to emissivity have an immediate effect on the total heat loss from the pipe.
Convection Heat Transfer
Turning our attention to convection heat transfer, this mode is characterized by the movement of fluid, such as air, that carries heat away from the surface. There are two types of convection: natural and forced. Natural convection arises due to temperature-induced density gradients in the fluid, causing it to move without any external forces. Forced convection, on the other hand, occurs when an external influence, like a fan or wind, causes the fluid to move over the surface.

In the exercise, both quiescent air (natural convection) and crosswind conditions (forced convection) were considered. The equation \(q_{conv} = h A (T_s - T_a)\) was used to calculate convection heat loss, where \(h\) is the heat transfer coefficient, dependent on the type of convection occurring. For natural convection, the formula \(h = \frac{k}{L}\text{Nu}\) was applied, and in the case of a cross-wind with a velocity of 10 m/s, the Dittus-Boelter equation was used to calculate the Nusselt number, thus determining \(h\) for forced convection.

This distinction is important as the two scenarios affect the rate of heat transfer differently, with forced convection typically resulting in higher heat transfer rates due to greater fluid movement. Consequently, assessing convection heat loss under different conditions is essential in understanding the overall heat loss from the pipe.
Emissivity Changes
Emissivity is a surface characteristic that measures how efficiently a material radiates energy compared to a perfect blackbody. It is crucial to understand that emissivity changes can profoundly impact radiation heat transfer and thus the total heat loss from an object. In the given exercise, the effects of emissivity changes on heat loss from an insulated pipe are investigated.

The aluminum foil that initially has a low emissivity of 0.12 undergoes degradation, with its emissivity increasing to 0.36. Such changes generally occur due to environmental factors like the presence of chlorine, leading to a surface that is less reflective and more effective at radiating heat.

As the equation for radiation heat transfer \(q_{rad}\) includes emissivity \(\epsilon\) as a variable, an increase leads to more significant heat loss. It is important to note that the emissivity of a surface can be affected by various factors, including texture, coating, and oxidation. When evaluating thermal insulation performance, particularly in harsh environments, factoring in the potential changes to surface emissivity over time is essential for accurate predictions of energy efficiency and heat loss.

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Most popular questions from this chapter

A household oven door of \(0.5-\mathrm{m}\) height and \(0.7-\mathrm{m}\) width reaches an average surface temperature of \(32^{\circ} \mathrm{C}\) during operation. Estimate the heat loss to the room with ambient air at \(22^{\circ} \mathrm{C}\). If the door has an emissivity of \(1.0\) and the surroundings are also at \(22^{\circ} \mathrm{C}\), comment on the heat loss by free convection relative to that by radiation.

A solar collector design consists of an inner tube enclosed concentrically in an outer tube that is transparent to solar radiation. The tubes are thin walled with inner and outer diameters of \(0.10\) and \(0.15 \mathrm{~m}\), respectively. The annular space between the tubes is completely enclosed and filled with air at atmospheric pressure. Under operating conditions for which the inner and outer tube surface temperatures are 70 and \(30^{\circ} \mathrm{C}\), respectively, what is the convective heat loss per meter of tube length across the air space?

9.27 The vertical rear window of an automobile is of thickness \(L=8 \mathrm{~mm}\) and height \(H=0.5 \mathrm{~m}\) and contains fine-meshed heating wires that can induce nearly uniform volumetric heating, \(\dot{q}\left(\mathrm{~W} / \mathrm{m}^{3}\right)\). (a) Consider steady-state conditions for which the interior surface of the window is exposed to quiescent air at \(10^{\circ} \mathrm{C}\), while the exterior surface is exposed to air at \(-10^{\circ} \mathrm{C}\) moving in parallel flow over the surface with a velocity of \(20 \mathrm{~m} / \mathrm{s}\). Determine the volumetric heating rate needed to maintain the interior window surface at \(T_{s, i}=15^{\circ} \mathrm{C}\). (b) The interior and exterior window temperatures, \(T_{s, i}\) and \(T_{s, \rho}\), depend on the compartment and ambient temperatures, \(T_{\infty, i}\) and \(T_{\infty, p}\), as well as on the velocity \(u_{\infty}\) of air flowing over the exterior surface and the volumetric heating rate \(\dot{q}\). Subject to the constraint that \(T_{s, i}\) is to be maintained at \(15^{\circ} \mathrm{C}\), we wish to develop guidelines for varying the heating rate in response to changes in \(T_{\infty,}, T_{\infty \rho,}\), and/or \(u_{\infty}\). If \(T_{\infty, i}\) is maintained at \(10^{\circ} \mathrm{C}\), how will \(\dot{q}\) and \(T_{s, \rho}\) vary with \(T_{\infty, o}\) for \(-25 \leq T_{\infty,,} \leq 5^{\circ} \mathrm{C}\) and \(u_{\infty}=10,20\), and \(30 \mathrm{~m} / \mathrm{s}\) ? If a constant vehicle speed is maintained, such that \(u_{\infty}=30 \mathrm{~m} / \mathrm{s}\), how will \(\dot{q}\) and \(T_{s, o}\) vary with \(T_{\infty, i}\) for \(5 \leq T_{\infty, i} \leq 20^{\circ} \mathrm{C}\) and \(T_{\infty, o}=-25,-10\), and \(5^{\circ} \mathrm{C}\) ?

The space between the panes of a double-glazed window can be filled with either air or carbon dioxide at atmospheric pressure. The window is \(1.5 \mathrm{~m}\) high and the spacing between the panes can be varied. Develop an analysis to predict the convection heat transfer rate across the window as a function of pane spacing and determine, under otherwise identical conditions, whether air or carbon dioxide will yield the smaller rate. Illustrate the results of your analysis for two surface-temperature conditions: winter \(\left(-10^{\circ} \mathrm{C}, 20^{\circ} \mathrm{C}\right)\) and summer \(\left(35^{\circ} \mathrm{C}, 25^{\circ} \mathrm{C}\right)\).

An aluminum alloy (2024) plate, heated to a uniform temperature of \(227^{\circ} \mathrm{C}\), is allowed to cool while vertically suspended in a room where the ambient air and surroundings are at \(27^{\circ} \mathrm{C}\). The plate is \(0.3 \mathrm{~m}\) square with a thickness of \(15 \mathrm{~mm}\) and an emissivity of \(0.25\). (a) Develop an expression for the time rate of change of the plate temperature, assuming the temperature to be uniform at any time. (b) Determine the initial rate of cooling (K/s) when the plate temperature is \(227^{\circ} \mathrm{C}\). (c) Justify the uniform plate temperature assumption. (d) Compute and plot the temperature history of the plate from \(t=0\) to the time required to reach a temperature of \(30^{\circ} \mathrm{C}\). Compute and plot the corresponding variations in the convection and radiation heat transfer rates.

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