/*! 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 A sphere \(\left(k=185 \mathrm{~... [FREE SOLUTION] | 91Ó°ÊÓ

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A sphere \(\left(k=185 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \alpha=7.25 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}\right)\) of \(30-\mathrm{mm}\) diameter whose surface is diffuse and gray with an emissivity of \(0.8\) is placed in a large oven whose walls are of uniform temperature at \(600 \mathrm{~K}\). The temperature of the air in the oven is \(400 \mathrm{~K}\), and the convection heat transfer coefficient between the sphere and the oven air is \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) Determine the net heat transfer to the sphere when its temperature is \(300 \mathrm{~K}\). (b) What will be the steady-state temperature of the sphere? (c) How long will it take for the sphere, initially at \(300 \mathrm{~K}\), to come within \(20 \mathrm{~K}\) of the steady-state temperature? (d) For emissivities of \(0.2,0.4\), and \(0.8\), plot the elapsed time of part (c) as a function of the convection coefficient for \(10 \leq h \leq 25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\).

Short Answer

Expert verified
(a) The net heat transfer to the sphere when its temperature is 300 K is \(Q_{net} = 1.025W\). (b) The steady-state temperature of the sphere is \(T_{steady} \approx 368.93 K\). (c) It takes approximately 676.48 seconds for the sphere to come within 20 K of the steady-state temperature. (d) For emissivities of 0.2, 0.4, and 0.8, the elapsed time to reach 20 K of the steady-state temperature decreases as the convection coefficient increases. The higher the emissivity, the faster the sphere reaches the desired temperature.

Step by step solution

01

(a) Calculate Net Heat Transfer

To calculate the net heat transfer to the sphere, we need to consider both convection and radiation heat transfers. Let's find the net heat transfer when the sphere's temperature is 300 K. Convection heat transfer, \(Q_{conv}\), can be calculated using the formula: \[Q_{conv} = hA(T_{air} - T_{sphere})\] Radiation heat transfer, \(Q_{rad}\), can be calculated using the formula: \[Q_{rad} = \epsilon A \sigma (T_{oven}^4 - T_{sphere}^4)\] Net heat transfer, \(Q_{net} = Q_{conv} + Q_{rad}\) Given: \(T_{air} = 400 K, T_{oven} = 600 K, T_{sphere} = 300 K, \epsilon = 0.8, h=15 \frac{W}{m^2K}\) Surface area of the sphere, \(A = 4\pi r^2\), with radius \(r=0.015m\). Now we can substitute values to calculate net heat transfer.
02

(b) Steady-state Temperature of the Sphere

To find the steady-state temperature, we need to solve for the temperature at which the sum of convection and radiation heat transfers equals zero. This means that \(Q_{net} = 0\). To find the temperature \(T_{steady}\), first set up the equation with unknown temperature \(T_{steady}\) and solve for \(T_{steady}\).
03

(c) Time to reach 20 K of Steady-state Temperature

To calculate the time it takes for the sphere to come within 20 K of the steady-state temperature, we'll use the following equation for unsteady heat conduction in a spherical solid: \[\frac{T - T_{steady}}{T_0 - T_{steady}} = e^{-\frac{4\pi k \alpha t}{(4 \pi r^3)\rho C_p}}\] We need to solve for time, \(t\), when \(T = T_{steady} - 20K\). Once we have the equation set up, we will solve for \(t\).
04

(d) Elapsed time for different emissivities

For emissivities 0.2, 0.4, and 0.8, we will plot the elapsed time of part (c) as a function of the convection coefficient for \(10 \leq h \leq 25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). First, we need to calculate the elapsed time for each emissivity value and convection coefficient value. We'll use the same equation from part (c), with different emissivity values. Once we have the elapsed time for each case, we will plot the data on a graph with the convection coefficient on the x-axis and the elapsed time on the y-axis. Each emissivity value will have its line to represent the relationship between the elapsed time and convection coefficient. By analyzing the plot, we can understand how the elapsed time changes as a function of the convection coefficient for different emissivities.

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Key Concepts

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

Convection Heat Transfer
When we talk about convection heat transfer, we are referring to the movement of heat through a fluid (which can be a liquid or a gas) caused by fluid motion. In our exercise, when the air in the oven that surrounds the sphere moves, it carries heat with it, effectively transferring energy from the hot oven air to the cooler sphere. This process can be described by the convection heat transfer equation:
\[ Q_{conv} = hA(T_{air} - T_{sphere}) \]
where \( Q_{conv} \) is the convection heat transfer rate, \( h \) is the convection heat transfer coefficient, \( A \) is the surface area of the sphere, \( T_{air} \) is the temperature of the oven air, and \( T_{sphere} \) is the temperature of the sphere. To maximize understanding of this concept, envision the air molecules as tiny messengers, carrying energy from one place to another within the oven. Imagine putting your hand above a boiling pot of water and feeling the heat rise—this is a tangible example of convection heat transfer at work.
Radiation Heat Transfer
Besides convection, there's another important form of heat transfer to discuss: radiation heat transfer. This is the energy transmitted by electromagnetic waves, and it doesn't require a medium, meaning it can even occur in a vacuum. The energy is carried by photons and can be emitted by any object with a temperature above absolute zero. Our exercise deals with this when considering the interaction of the sphere with the radiant energy from the oven walls.
The equation for radiation heat transfer is as follows:
\[ Q_{rad} = \epsilon A \sigma (T_{oven}^4 - T_{sphere}^4) \]
Here, \( Q_{rad} \) is the radiation heat transfer rate, \( \epsilon \) is the emissivity of the sphere's surface, \( A \) is the surface area, \( \sigma \) is the Stefan-Boltzmann constant, and \( T_{oven} \) and \( T_{sphere} \) are the temperatures of the oven walls and the sphere, respectively. The emissivity is indicative of how well an object can emit (and absorb) radiation; a perfect black body would have an emissivity of 1. Our sphere, with an emissivity of 0.8, is a good emitter and absorber of radiation, though not perfect. To visualize this, think of how you can feel the warmth of the sun on your skin even on a cold day—that's the radiation heat transfer in action!
Steady-State Temperature
Now, let's shift our focus to the concept of steady-state temperature, which is a crucial point in understanding heat transfer in systems that reach equilibrium. In steady state, the temperature of the system doesn't change with time, which implies that the heat entering the system is equal to the heat leaving it. In our sphere's case, this means that the heat absorbed through convection and radiation from the oven air and walls is equal to any heat the sphere might emit or transfer to its surroundings.
When the exercise asks for the steady-state temperature of the sphere, it's asking us to find the temperature at which the net heat transfer is zero. Mathematically:
\[ Q_{net} = Q_{conv} + Q_{rad} = 0 \]
To solve for the sphere's steady-state temperature, \(T_{steady}\), we would set up the above equation with \(T_{steady}\) in place of \(T_{sphere}\) and solve accordingly. At steady state, the temperature of the sphere would stop changing, meaning the energy it receives and emits has reached a balance.
Unsteady Heat Conduction
Lastly, we'll discuss the concept of unsteady heat conduction, which occurs when temperatures within a material change over time. It's also known as transient heat conduction. Our sphere doesn’t reach its steady state immediately; it goes through a transient phase where its temperature gradually approaches the steady state. During this period, we need to understand how the temperature at any point within the sphere changes with time. This is described by transient heat conduction equations.
In this part of the exercise, we calculate how long it will take for the sphere to get within 20 K of the steady-state temperature. This involves the following equation, which models the temperature change over time in a spherical object:
\[ \frac{T - T_{steady}}{T_0 - T_{steady}} = e^{-\frac{4\pi k \alpha t}{(4 \pi r^3)\rho C_p}} \]
Here, \( T \) is the sphere's temperature at time \( t \), \( T_{steady} \) is the steady-state temperature, \( T_0 \) is the initial temperature of the sphere, \( k \) is the thermal conductivity, \( \alpha \) is the thermal diffusivity, \( r \) is the radius, \( \rho \) is the density, and \( C_p \) is the specific heat capacity. Solving this equation for \( t \) when \( T \) is a specific value (in this case, \( T_{steady} - 20 \text{K} \)) gives us the time needed for the sphere to nearly reach its steady-state. Imagine baking a potato in an oven; it doesn’t heat up instantaneously but rather takes time to reach a uniform temperature throughout—that’s unsteady heat conduction at work.

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Most popular questions from this chapter

The absorber plate of a solar collector may be coated with an opaque material for which the spectral, directional absorptivity is characterized by relations of the form $$ \begin{array}{ll} \alpha_{\lambda, \dot{\theta}}(\lambda, \theta)=\alpha_{1} \cos \theta & \lambda<\lambda_{c} \\ \alpha_{\lambda, \theta}(\lambda, \theta)=\alpha_{2} & \lambda>\lambda_{c} \end{array} $$ The zenith angle \(\theta\) is formed by the sun's rays and the plate normal, and \(\alpha_{1}\) and \(\alpha_{2}\) are constants. (a) Obtain an expression for the total, hemispherical absorptivity, \(\alpha_{S}\), of the plate to solar radiation incident at \(\theta=45^{\circ}\). Evaluate \(\alpha_{5}\) for \(\alpha_{1}=0.93, \alpha_{2}=\) \(0.25\), and a cut-off wavelength of \(\lambda_{c}=2 \mu \mathrm{m}\). (b) Obtain an expression for the total, hemispherical emissivity \(\varepsilon\) of the plate. Evaluate \(\varepsilon\) for a plate temperature of \(T_{p}=60^{\circ} \mathrm{C}\) and the prescribed values of \(\alpha_{1}, \alpha_{2}\), and \(\lambda_{c}\). (c) For a solar flux of \(q_{s}^{\prime \prime}=1000 \mathrm{~W} / \mathrm{m}^{2}\) incident at \(\theta=45^{\circ}\) and the prescribed values of \(\alpha_{1}, \alpha_{2}, \lambda_{c}\), and \(T_{p}\), what is the net radiant heat flux, \(q_{\text {net }}^{\prime \prime}\), to the plate? (d) Using the prescribed conditions and the Radiation/ Band Emission Factor option in the Tools section of \(I H T\) to evaluate \(F_{\left(0 \rightarrow \lambda_{j}\right)}\), explore the effect of \(\lambda_{c}\) on \(\alpha_{S}, \varepsilon\), and \(q_{\text {net }}^{N}\) for the wavelength range \(0.7 \leq \lambda_{c} \leq 5 \mu \mathrm{m}\).

The oxidized-aluminum wing of an aircraft has a chord length of \(L_{c}=4 \mathrm{~m}\) and a spectral, hemispherical emissivity characterized by the following distribution. (a) Consider conditions for which the plane is on the ground where the air temperature is \(27^{\circ} \mathrm{C}\), the solar irradiation is \(800 \mathrm{~W} / \mathrm{m}^{2}\), and the effective sky temperature is \(270 \mathrm{~K}\). If the air is quiescent, what is the temperature of the top surface of the wing? The wing may be approximated as a horizontal, flat plate. (b) When the aircraft is flying at an elevation of approximately \(9000 \mathrm{~m}\) and a speed of \(200 \mathrm{~m} / \mathrm{s}\), the air temperature, solar irradiation, and effective sky temperature are \(-40^{\circ} \mathrm{C}, 1100 \mathrm{~W} / \mathrm{m}^{2}\), and \(235 \mathrm{~K}\), respectively. What is the temperature of the wing's top surface? The properties of the air may be approximated as \(\rho=0.470 \mathrm{~kg} / \mathrm{m}^{3}, \mu=1.50 \times\) \(10^{-5} \mathrm{~N} \cdot \mathrm{s} / \mathrm{m}^{2}, k=0.021 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and \(P r=0.72\).

Consider an opaque, gray surface whose directional absorptivity is \(0.8\) for \(0 \leq \theta \leq 60^{\circ}\) and \(0.1\) for \(\theta>60^{\circ}\). The surface is horizontal and exposed to solar irradiation comprised of direct and diffuse components. (a) What is the surface absorptivity to direct solar radiation that is incident at an angle of \(45^{\circ}\) from the normal? What is the absorptivity to diffuse irradiation? (b) Neglecting convection heat transfer between the surface and the surrounding air, what would be the equilibrium temperature of the surface if the direct and diffuse components of the irradiation were 600 and \(100 \mathrm{~W} / \mathrm{m}^{2}\), respectively? The back side of the surface is insulated.

Consider Problem \(4.51 .\) (a) The students are each given a flat, fot-surface silver mirror with which they collectively irradiate the wooden ship at location B. The reflection from the mirror is specular, and the silver's reflectivity is \(0.98\). The solar irradiation of each mirror, perpendicular to the direction of the sun's rays, is \(G_{S}=1000 \mathrm{~W} / \mathrm{m}^{2}\). How many students are needed to conduct the experiment if the solar absorptivity of the wood is \(\alpha_{w}=0.80\) and the mirror is oriented at an angle of \(45^{\circ}\) from the direction of \(G_{S}\) ? (b) If the students are given second-surface mirrors that consist of a sheet of plain glass that has polished silver on its back side, how many students are needed to conduct the experiment? Hint: See Problem \(12.62 .\)

A thermocouple inserted in a 4-mm-diameter stainless steel tube having a diffuse, gray surface with an emissivity of \(0.4\) is positioned horizontally in a large airconditioned room whose walls and air temperature are 30 and \(20^{\circ} \mathrm{C}\), respectively. (a) What temperature will the thermocouple indicate if the air is quiescent? (b) Compute and plot the thermocouple measurement error as a function of the surface emissivity for \(0.1 \leq \varepsilon \leq 1.0\).

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