/*! 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 17 Small spherical particles of dia... [FREE SOLUTION] | 91Ó°ÊÓ

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Small spherical particles of diameter \(D=50 \mu \mathrm{m}\) contain a fluorescent material that, when irradiated with white light, emits at a wavelength corresponding to the material's temperature. Hence the color of the particle varies with its temperature. Because the small particles are neutrally buoyant in liquid water, a researcher wishes to use them to measure instantaneous local water temperatures in a turbulent flow by observing their emitted color. If the particles are characterized by a density, specific heat, and thermal conductivity of \(\rho=999 \mathrm{~kg} / \mathrm{m}^{3}\), \(k=1.2 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and \(c_{p}=1200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), respectively, determine the time constant of the particles. Hint: Since the particles travel with the flow, heat transfer between the particle and the fluid occurs by conduction. Assume lumped capacitance behavior.

Short Answer

Expert verified
The time constant of the small spherical particles containing fluorescent material can be calculated using the lumped capacitance equation and given properties. First, find the volume and surface area of the particles using their diameter. Then, relate the convective heat transfer coefficient to the thermal conductivity. Finally, calculate the time constant using the lumped capacitance equation. The time constant of the particles is approximately \(1.180 \times 10^{-5}\) seconds.

Step by step solution

01

Understand and list given information

The problem states the following information: - The diameter of the particles: \(D = 50 \mu m\) - The density: \(\rho = 999 \frac{kg}{m^3}\) - The thermal conductivity: \(k = 1.2 \frac{W}{m \cdot K}\) - The specific heat: \(c_p = 1200 \frac{J}{kg \cdot K}\) - The heat transfer between the particle and the fluid occurs by conduction - Lumped capacitance behavior is assumed
02

Calculate time constant using the lumped capacitance equation

We can use the lumped capacitance equation to find the time constant: \(t_c = \frac{V \rho c_p}{hA}\) Where: \(t_c =\) time constant \(V =\) volume of the particle \(\rho =\) density \(c_p =\) specific heat \(h =\) convective heat transfer coefficient \(A =\) surface area of the particles First, we need to calculate the volume and the surface area of the particles.
03

Calculate the volume and the surface area of the particles

We know that the particles are spheres, so the volume (\(V\)) and the surface area (\(A\)) of a sphere with diameter \(D\) can be found using the following equations: \(V = \frac{4}{3} \pi r^3\) \(A = 4 \pi r^2\) Where: \(r =\) radius of the sphere (\(\frac{D}{2}\)) Let's find the radius, volume and surface area of the particles: Radius (in meters): \(r = \frac{D}{2} = \frac{50 \times 10^{-6} m}{2} = 25 \times 10^{-6} m\) Volume: \(V = \frac{4}{3} \pi (25 \times 10^{-6})^3 = 6.544 \times 10^{-14} m^3\) Surface area: \(A = 4 \pi (25 \times 10^{-6})^2 = 7.854 \times 10^{-9} m^2\)
04

Relate the convective heat transfer coefficient to thermal conductivity

Since the heat transfer between the particle and the fluid occurs by conduction, we can assume that the conductive heat transfer is equal to the convective heat transfer. Therefore, we can write the following relation: \(hL = k\) Where: \(L =\) characteristic length \(k =\) thermal conductivity For a sphere, the characteristic length can be defined as the radius: \(L = r\) Now, let's calculate the convective heat transfer coefficient using this relation: \(h = \frac{k}{r} = \frac{1.2 \frac{W}{m \cdot K}}{25 \times 10^{-6} m} = 48000 \frac{W}{m^2 \cdot K}\)
05

Calculate the time constant

Now that we have all the necessary values, we can calculate the time constant using the lumped capacitance equation: \(t_c = \frac{V \rho c_p}{hA} = \frac{(6.544 \times 10^{-14} \frac{m^3})(999 \frac{kg}{m^3})(1200 \frac{J}{kg \cdot K})}{(48000 \frac{W}{m^2 \cdot K})(7.854 \times 10^{-9} m^2)} = 1.180 \times 10^{-5} s\) The time constant of the particles is approximately \(1.180 \times 10^{-5}\) seconds.

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Key Concepts

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

Lumped Capacitance Method
Understanding the concept of the lumped capacitance method is crucial for analyzing heat transfer in scenarios where the temperature within an object can be assumed to be uniform. This technique simplifies the complex heat transfer equations by treating the object as a single node with uniform temperature. When can we use this method? It is applicable when the Biot number, a dimensionless parameter, is very small (typically less than 0.1), indicating that the conductive resistance inside the object is much smaller than the convective resistance on the object's surface.

To apply the lumped capacitance method, one must first establish the object's thermal properties, such as its density \( \rho \), specific heat \( c_p \), volume \( V \), and surface area \( A \). The thermal response of the object is then characterized by the time constant \( t_c \) — an indicator of how quickly the object will respond to changes in its thermal environment.

In the exercise, we calculated the time constant using the formula:\[ t_c = \frac{V \rho c_p}{hA} \]where \( h \) is the convective heat transfer coefficient. The small spherical particles used in the exercise have properties that allow the assumption of lumped capacitance behavior, thus enabling an efficient way to measure instantaneous water temperatures through the particles' color change.
Convective Heat Transfer Coefficient
The convective heat transfer coefficient \( h \) plays a pivotal role in characterizing the rate of heat transfer between a surface and a fluid flowing past it. It's a measure of the convective heat transfer per unit area and per unit temperature difference between the surface and the fluid. This coefficient depends on various factors, such as the type of fluid, flow properties, and the surface geometry.

In turbulent flow, the convective heat transfer coefficient is affected by the eddies and swirls that enhance the mixing of the fluid, thus increasing \( h \). This phenomenon is quite different from laminar flow, where the heat transfer is often lower due to the orderly flow layers with minimal mixing.

As seen in the exercise, to find \( h \) we used the relationship that equates convective heat transfer to conductive heat transfer within the fluid, since our particles move with the flow and heat transfer between the particle and the fluid occurs via conduction. The formula used to relate the convective heat transfer coefficient to the thermal conductivity \( k \) considering the characteristic length \( L \) (which is the radius for a sphere) is:\[ h = \frac{k}{L} = \frac{k}{r} \]This relation simplifies the determination of \( h \) when thermal conductivity and characteristic length are known, as they are for the spherical particles in the exercise.
Thermal Conductivity
At the heart of conduction heat transfer is the material property known as thermal conductivity \( k \). It represents the ability of a material to conduct heat and is defined as the rate at which heat passes through a material with a given area and temperature gradient. Higher thermal conductivity means that the material is a better conductor of heat.

For the given exercise, knowing the thermal conductivity of the particles allows us to connect conductive heat transfer in the material to the convective heat transfer in the surrounding fluid. The thermal conductivity \( k \) aids in the determination of the particles' temperature response to the environment, given as a part of their physical properties. \( k = 1.2 \frac{W}{m \cdot K} \) for the small spherical particle indicates a relatively low thermal conductivity suggesting that they can quickly reach thermal equilibrium with the surrounding fluid.

Ultimately, understanding thermal conductivity is key for various applications, from engineering thermal management systems to designing materials for efficient heat dissipation or insulation. It is a cornerstone in calculating the convective heat transfer coefficient, as shown in the exercise, linking material properties to heat transfer analysis.

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Most popular questions from this chapter

A spherical vessel used as a reactor for producing pharmaceuticals has a 5 -mm-thick stainless steel wall \((k=17 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) and an inner diameter of \(D_{i}=1.0 \mathrm{~m}\). During production, the vessel is filled with reactants for which \(\rho=1100 \mathrm{~kg} / \mathrm{m}^{3}\) and \(c=2400 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), while exothermic reactions release energy at a volumetric rate of \(\dot{q}=10^{4} \mathrm{~W} / \mathrm{m}^{3}\). As first approximations, the reactants may be assumed to be well stirred and the thermal capacitance of the vessel may be neglected. (a) The exterior surface of the vessel is exposed to ambient air \(\left(T_{\infty}=25^{\circ} \mathrm{C}\right)\) for which a convection coefficient of \(h=6 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) may be assumed. If the initial temperature of the reactants is \(25^{\circ} \mathrm{C}\), what is the temperature of the reactants after \(5 \mathrm{~h}\) of process time? What is the corresponding temperature at the outer surface of the vessel? (b) Explore the effect of varying the convection coefficient on transient thermal conditions within the reactor. A spherical vessel used as a reactor for producing pharmaceuticals has a 5 -mm-thick stainless steel wall \((k=17 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) and an inner diameter of \(D_{i}=1.0 \mathrm{~m}\). During production, the vessel is filled with reactants for which \(\rho=1100 \mathrm{~kg} / \mathrm{m}^{3}\) and \(c=2400 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), while exothermic reactions release energy at a volumetric rate of \(\dot{q}=10^{4} \mathrm{~W} / \mathrm{m}^{3}\). As first approximations, the reactants may be assumed to be well stirred and the thermal capacitance of the vessel may be neglected. (a) The exterior surface of the vessel is exposed to ambient air \(\left(T_{\infty}=25^{\circ} \mathrm{C}\right)\) for which a convection coefficient of \(h=6 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) may be assumed. If the initial temperature of the reactants is \(25^{\circ} \mathrm{C}\), what is the temperature of the reactants after \(5 \mathrm{~h}\) of process time? What is the corresponding temperature at the outer surface of the vessel? (b) Explore the effect of varying the convection coefficient on transient thermal conditions within the reactor.

Consider the thick slab of copper in Example 5.12, which is initially at a uniform temperature of \(20^{\circ} \mathrm{C}\) and is suddenly exposed to a net radiant flux of \(3 \times 10^{5} \mathrm{~W} / \mathrm{m}^{2}\). Use the Finite-Difference Equations/ One-Dimensional/Transient conduction model builder of \(I H T\) to obtain the implicit form of the finite-difference equations for the interior nodes. In your analysis, use a space increment of \(\Delta x=37.5 \mathrm{~mm}\) with a total of 17 nodes (00-16), and a time increment of \(\Delta t=1.2 \mathrm{~s}\). For the surface node 00 , use the finite-difference equation derived in Section 2 of the Example. (a) Calculate the 00 and 04 nodal temperatures at \(t=120 \mathrm{~s}\), that is, \(T(0,120 \mathrm{~s})\) and \(T(0.15 \mathrm{~m}, 120 \mathrm{~s})\), and compare the results with those given in Comment 1 for the exact solution. Will a time increment of \(0.12 \mathrm{~s}\) provide more accurate results? (b) Plot temperature histories for \(x=0,150\), and \(600 \mathrm{~mm}\), and explain key features of your results.

The 150 -mm-thick wall of a gas-fired furnace is constructed of fireclay brick \((k=1.5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=2600\) \(\left.\mathrm{kg} / \mathrm{m}^{3}, c_{p}=1000 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) and is well insulated at its outer surface. The wall is at a uniform initial temperature of \(20^{\circ} \mathrm{C}\), when the burners are fired and the inner surface is exposed to products of combustion for which \(T_{\infty}=950^{\circ} \mathrm{C}\) and \(h=100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) How long does it take for the outer surface of the wall to reach a temperature of \(750^{\circ} \mathrm{C}\) ? (b) Plot the temperature distribution in the wall at the foregoing time, as well as at several intermediate times.

To determine which parts of a spider's brain are triggered into neural activity in response to various optical stimuli, researchers at the University of Massachusetts Amherst desire to examine the brain as it is shown images that might evoke emotions such as fear or hunger. Consider a spider at \(T_{i}=20^{\circ} \mathrm{C}\) that is shown a frightful scene and is then immediately immersed in liquid nitrogen at \(T_{\infty}=77 \mathrm{~K}\). The brain is subsequently dissected in its frozen state and analyzed to determine which parts of the brain reacted to the stimulus. Using your knowledge of heat transfer, determine how much time elapses before the spider's brain begins to freeze. Assume the brain is a sphere of diameter \(D_{b}=1 \mathrm{~mm}\), centrally located in the spider's cephalothorax, which may be approximated as a spherical shell of diameter \(D_{c}=3 \mathrm{~mm}\). The brain and cephalothorax properties correspond to those of liquid water. Neglect the effects of the latent heat of fusion and assume the heat transfer coefficient is \(h=100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\).

Thermal energy storage systems commonly involve a packed bed of solid spheres, through which a hot gas flows if the system is being charged, or a cold gas if it is being discharged. In a charging process, heat transfer from the hot gas increases thermal energy stored within the colder spheres; during discharge, the stored energy decreases as heat is transferred from the warmer spheres to the cooler gas. Consider a packed bed of \(75-\mathrm{mm}\)-diameter aluminum spheres \(\left(\rho=2700 \mathrm{~kg} / \mathrm{m}^{3}, c=950 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k=\right.\) \(240 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) ) and a charging process for which gas enters the storage unit at a temperature of \(T_{g, i}=300^{\circ} \mathrm{C}\). If the initial temperature of the spheres is \(T_{i}=25^{\circ} \mathrm{C}\) and the convection coefficient is \(h=75 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), how long does it take a sphere near the inlet of the system to accumulate \(90 \%\) of the maximum possible thermal energy? What is the corresponding temperature at the center of the sphere? Is there any advantage to using copper instead of aluminum?

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