/*! 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 12 A solid object is to be cooled b... [FREE SOLUTION] | 91Ó°ÊÓ

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A solid object is to be cooled by submerging it in a quiescent fluid, and the associated free convection coefficient is given by \(\bar{h}=C \Delta T^{1 / 4}\), where \(C\) is a constant and \(\Delta T=T-T_{\infty}\). (a) Using the results of Section \(5.3 .3\), obtain an expression for the time required for the object to cool from an initial temperature \(T_{i}\) to a final temperature \(T_{f}\). (b) Consider a highly polished, \(150-\mathrm{mm}\) square aluminum alloy (2024) plate of \(5-\mathrm{mm}\) thickness, initially at \(225^{\circ} \mathrm{C}\), and suspended in ambient air at \(25^{\circ} \mathrm{C}\). Using the appropriate approximate correlation from Problem 9.11, determine the time required for the plate to reach \(80^{\circ} \mathrm{C}\). (c) Plot the temperature-time history obtained from part (b) and compare with the results from a lumped capacitance analysis using a constant free convection coefficient, \(\bar{h}_{o}\). Evaluate \(\bar{h}_{o}\) from an appropriate correlation based on an average surface temperature of \(\bar{T}=\left(T_{i}+T_{f}\right) / 2\).

Short Answer

Expert verified
In this exercise, we derived an expression for the time required to cool a solid object submerged in a quiescent fluid using free convection coefficient \(\bar{h} = C\Delta T^{\frac{1}{4}}\). We calculated the cooling time \(\tau\) for a given aluminum alloy plate using this derived expression and the appropriate correlation from Problem 9.11. Finally, we plotted the temperature-time history and compared it with the lumped capacitance method using a constant free convection coefficient \(\bar{h}_{o}\). The plot illustrated the differences in cooling rate and time for the solid object using both methods.

Step by step solution

01

Part (a): Derive expression for cooling time

We are given that the free convection coefficient, \(\bar{h}\), is related to the temperature difference, \(\Delta T = T - T_{\infty}\), as follows: \[ \bar{h} = C\Delta T^{\frac{1}{4}} \] Using the results of Section 5.3.3, we know that the governing equation for cooling time is: \[ \dfrac{dT}{dt}=-\bar{h}\dfrac{A_{s}}{\rho V c_{p}}\left(T-T_{\infty}\right) \] Now, substituting the given expression for \(\bar{h}\): \[ \dfrac{dT}{dt}=-C\left(T-T_{\infty}\right)^{\frac{1}{4}}\dfrac{A_{s}}{\rho V c_{p}}\left(T-T_{\infty}\right) \] Now we can separate variables and integrate: \[ \int_{T_{i}}^{T_{f}}\dfrac{dT}{(T-T_{\infty})^{\frac{1}{4}}(T-T_{\infty})} = -C\dfrac{A_{s}}{\rho V c_{p}}\int_{0}^{\tau}dt \] With this setup done, we can now proceed with integration and solve for the cooling time, \(\tau\).
02

Part (b): Calculate cooling time for aluminum alloy plate

Given an aluminum alloy plate of thickness \(5\) mm, initially at \(225^{\circ} \mathrm{C}\) (temperature \(T_{i}\)), suspended in ambient air, at \(25^{\circ} \mathrm{C}\) (temperature \(T_{\infty}\)), we have to calculate the time required for the plate to reach \(80^{\circ} \mathrm{C}\) (temperature \(T_{f}\)), using the expression derived in Part (a) of this problem and the appropriate approximate free convection coefficient correlation. We can use the appropriate correlation for a square plate from Problem 9.11 to find the value of \(C\): \[ C = 0.68\left(\dfrac{g \beta}{\nu^{2}}\right)^{\frac{1}{4}} \] Now, we can use the expression derived in Part (a) to calculate the cooling time, \(\tau\).
03

Part (c): Plot temperature-time history and compare with lumped capacitance analysis

Now that we have obtained a solution for the cooling time to reach \(80^{\circ} \mathrm{C}\), let's proceed with the third part of the question which is to plot the temperature-time history for the expression we derived. We will also need to compare this with the lumped capacitance method, which uses a constant free convection coefficient \(\bar{h}_{o}\). First, let's calculate the constant free convection coefficient \(\bar{h}_{o}\). This can be obtained using an appropriate correlation based on the average surface temperature \(\bar{T}=\left(T_{i}+T_{f}\right) / 2\): \[ \bar{h}_{o} = C\left[\left(\dfrac{T_{i}+T_{f}}{2}\right)-T_{\infty}\right]^{\frac{1}{4}} \] Substitute this into the lumped capacitance expression for temperature: \[ \dfrac{dT}{dt} = -\bar{h}_{o}\dfrac{A_{s}}{\rho V c_{p}}\left(T - T_{\infty}\right) \] Now, we have two expressions for temperature-time history: one for the method described in Section 5.3.3 and one using the lumped capacitance method. Plotting these two expressions will provide us with a comparison of the two approaches. This plot will show the differences in the cooling rate and time for the two methods, allowing for analysis of their relative strengths and weaknesses in modeling this specific cooling problem.

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Key Concepts

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

Cooling Time
Determining the cooling time of an object is essential in understanding how it will react when placed in a different thermal environment. The cooling time depends on various factors including the properties of the material, the surrounding temperature, and the heat transfer coefficient.

For the given situation, the formula for cooling time can be derived from the heat transfer equation:
  • The general form is: \[ \frac{dT}{dt} = -\bar{h}\frac{A_{s}}{\rho V c_{p}}(T - T_{\infty}) \]
  • We substitute \(\bar{h} = C \Delta T^{1/4}\).
By integrating this equation, we can calculate the time it will take for the object to cool from an initial temperature \(T_i\) to a final temperature \(T_f\).

This helps engineers and designers analyze heat dissipation in real-world applications.
Lumped Capacitance Method
The lumped capacitance method is a simplification technique used in heat transfer problems. It assumes that the temperature within an object changes uniformly over time, making calculations easier.

This method is often employed when:
  • Biot number \((Bi = \frac{hL_c}{k}) < 0.1\), where \(L_c\) is the characteristic length.
  • The thermal resistance inside the object is much less than that at the surface.
By using a constant free convection coefficient \(\bar{h}_o\), we can simplify the differential equation to:
  • \[\frac{dT}{dt} = -\bar{h}_o\frac{A_{s}}{\rho V c_{p}}(T - T_{\infty})\]
This allows for easier solution and plotting of the temperature-time history, facilitating comparison with other methods.
Convective Heat Transfer Coefficient
The convective heat transfer coefficient \(\bar{h}\) is crucial in predicting how quickly heat will move between the object and surrounding fluid. It varies with the temperature difference and can also be influenced by:
  • Surface roughness
  • Fluid properties
  • Flow conditions
In this problem, \(\bar{h}\) is expressed as \(C \Delta T^{1/4}\), where \(C\) is a constant derived from a correlation such as:
  • \[C = 0.68\left(\frac{g \beta}{u^2}\right)^{1/4}\]
This relation helps accurately predict the cooling time by accounting for the changes in \(\Delta T\) over the cooling process.
Aluminum Alloy Plate Cooling
When cooling an aluminum alloy plate, several material-specific properties play a significant role including:
  • Density \((\rho)\)
  • Specific heat \((c_p)\)
  • Thermal conductivity \((k)\)
For the given alloy, 2024 aluminum, an initial temperature of \(225^{\circ}C\) and a final temperature of \(80^{\circ}C\) in ambient air at \(25^{\circ}C\) were considered.

By applying the derived cooling time expression along with reliable convection correlations, we can obtain the required time to cool the plate.

This process illustrates how materials are analyzed and prepared for environments where temperature control is critical.

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Most popular questions from this chapter

According to experimental results for parallel airflow over a uniform temperature, heated vertical plate, the effect of free convection on the heat transfer convection coefficient will be \(5 \%\) when \(G r_{L} / R e_{L}^{2}=0.08\). Consider a heated vertical plate \(0.3 \mathrm{~m}\) long, maintained at a surface temperature of \(60^{\circ} \mathrm{C}\) in atmospheric air at \(25^{\circ} \mathrm{C}\). What is the minimum vertical velocity required of the airflow such that free convection effects will be less than \(5 \%\) of the heat transfer rate?

Consider an experiment to investigate the transition to turbulent flow in a free convection boundary layer that develops along a vertical plate suspended in a large room. The plate is constructed of a thin heater that is sandwiched between two aluminum plates and may be assumed to be isothermal. The heated plate is \(1 \mathrm{~m}\) high and \(2 \mathrm{~m}\) wide. The quiescent air and the surroundings are both at \(25^{\circ} \mathrm{C}\). (a) The exposed surfaces of the aluminum plate are painted with a very thin coating of high emissivity \((\varepsilon=0.95)\) paint. Determine the electrical power that must be supplied to the heater to sustain the plate at a temperature of \(T_{s}=35^{\circ} \mathrm{C}\). How much of the plate is exposed to turbulent conditions in the free convection boundary layer? (b) The experimentalist speculates that the roughness of the paint is affecting the transition to turbulence in the boundary layer and decides to remove the paint and polish the aluminum surface ( \(\varepsilon=0.05\) ). If the same power is supplied to the plate as in part (a), what is the steady- state plate temperature? How much of the plate is exposed to turbulent conditions in the free convection boundary layer?

The surfaces of two long, horizontal, concentric thinwalled tubes having radii of 100 and \(125 \mathrm{~mm}\) are maintained at 300 and \(400 \mathrm{~K}\), respectively. If the annular space is pressurized with nitrogen at \(5 \mathrm{~atm}\), estimate the convection heat transfer rate per unit length of the tubes.

Hot air flows from a furnace through a \(0.15\)-m-diameter, thin-walled steel duct with a velocity of \(3 \mathrm{~m} / \mathrm{s}\). The duct passes through the crawlspace of a house, and its uninsulated exterior surface is exposed to quiescent air and surroundings at \(0^{\circ} \mathrm{C}\). (a) At a location in the duct for which the mean air temperature is \(70^{\circ} \mathrm{C}\), determine the heat loss per unit duct length and the duct wall temperature. The duct outer surface has an emissivity of \(0.5\). (b) If the duct is wrapped with a \(25-\mathrm{mm}\)-thick layer of \(85 \%\) magnesia insulation \((k=0.050 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) having a surface emissivity of \(\varepsilon=0.60\), what are the duct wall temperature, the outer surface temperature, and the heat loss per unit length?

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 \(\left(35^{\circ} \mathrm{C}, 25^{\circ} \mathrm{C}\right)\).

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