/*! 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 23 A steel strip of thickness \(\de... [FREE SOLUTION] | 91Ó°ÊÓ

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A steel strip of thickness \(\delta=12 \mathrm{~mm}\) is annealed by passing it through a large furnace whose walls are maintained at a temperature \(T_{w}\) corresponding to that of combustion gases flowing through the furnace \(\left(T_{w}=T_{\infty}\right)\). The strip, whose density, specific heat, thermal conductivity, and emissivity are \(\rho=7900 \mathrm{~kg} / \mathrm{m}^{3}\), \(c_{p}=640 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k=30 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and \(\varepsilon=0.7\), respectively, is to be heated from \(300^{\circ} \mathrm{C}\) to \(600^{\circ} \mathrm{C}\). (a) For a uniform convection coefficient of \(h=\) \(100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(T_{w}=T_{\infty}=700^{\circ} \mathrm{C}\), determine the time required to heat the strip. If the strip is moving at \(0.5 \mathrm{~m} / \mathrm{s}\), how long must the furnace be? (b) The annealing process may be accelerated (the strip speed increased) by increasing the environmental temperatures. For the furnace length obtained in part (a), determine the strip speed for \(T_{w}=T_{\infty}=\) \(850^{\circ} \mathrm{C}\) and \(T_{w}=T_{\infty}=1000^{\circ} \mathrm{C}\). For each set of environmental temperatures \(\left(700,850\right.\), and \(\left.1000^{\circ} \mathrm{C}\right)\), plot the strip temperature as a function of time over the range \(25^{\circ} \mathrm{C} \leq T \leq 600^{\circ} \mathrm{C}\). Over this range, also plot the radiation heat transfer coefficient, \(h_{r}\), as a function of time.

Short Answer

Expert verified
In summary, to determine the time required to heat the steel strip and corresponding furnace length, we considered heat transfer through convection and radiation, and established a differential energy balance equation. We then solved for the time and temperature evolution of the strip numerically. Based on this, we calculated strip speed for different environmental temperatures and analyzed the temperature and radiation heat transfer coefficient as functions of time.

Step by step solution

01

Express the heat transfer through convection and radiation

In order to heat up the strip, it receives heat from the environment through convection and radiation. First, let's state the formulas for the heat transfer rate by convection (\(q_c\)) and radiation (\(q_r\)). For convection: \(q_c = h \cdot A \cdot (T_w - T)\) For radiation: \(q_r = \varepsilon \cdot A \cdot \sigma \cdot (T_w^4 - T^4)\) Where: - h: convection coefficient - A: area of the strip - \(T_w\): temperature of the furnace walls - T: temperature of the strip - \(\varepsilon\): emissivity of the strip - \(\sigma\): Stephan-Boltzmann constant The total heat transfer rate, \(q_{total}\) is then: \(q_{total} = q_c + q_r\)
02

Determine the heat capacity of the strip and differential energy balance

Next, we need to express the energy accumulated by the strip while crossing the furnace, which will be defined by the heat capacity of the strip. Heat capacity of the steel strip: \(m = \rho \cdot \delta \cdot A\) The accumulated energy by the strip during the annealing process can be represented as the change in energy from the initial temperature (\(T_i\)) to the final temperature (\(T_f\)) with: \(\Delta E = m \cdot c_p (T_f - T_i)\) Now, we will write the differential energy balance equation for heating the strip: \(\frac{dq_{total}}{dt} = m \cdot c_p \cdot \frac{dT}{dt}\) This will allow us to determine the time and temperature evolution of the strip.
03

Solve for time and temperature evolution

We can solve the differential energy balance equation to find an expression for the time evolution of the strip's temperature. This mathematical expression can then be solved numerically to obtain the time required to heat the strip for different wall temperatures and environmental conditions. Additionally, once the time is found, we can determine the furnace length necessary for the annealing process to be successfully accomplished.
04

Solve for the strip speed and plot results

With the time found from step 3, we can then determine the strip speed for each environmental temperature. The strip speed \(v\) can be expressed as: \(v = \frac{L_{furnace}}{t}\) Where \(L_{furnace}\) is the furnace length and \(t\) is the time required for the annealing process. Finally, we can plot the strip temperature as a function of time for different environmental temperatures to analyze the behavior of the annealing process. Furthermore, the radiation heat transfer coefficient (\(h_r\)) can be plotted as a function of time. To do this, we will solve for the temperature evolution and strip speed numerically for each set of environmental temperatures (\(700^{\circ}\), \(850^{\circ}\), and \(1000^{\circ}\)) and analyze the plot results.

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Key Concepts

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

Convection Heat Transfer
Understanding how heat moves is critical to grasping the annealing process, a heat treatment that alters the microstructure of a material to change its mechanical or electrical properties. One of the primary mechanisms of heat transfer involved in annealing is convection heat transfer. Convection is the transport of heat by the movement of a fluid — which may be a liquid or a gas — over a surface. In the context of our steel strip annealing example, the fluid is the combustion gases flowing through the furnace, transferring heat to the strip as it passes through.

To quantify this transfer, we use the convection heat transfer rate equation:
\(q_c = h \times A \times (T_w - T)\).

Here, \(q_c\) represents the rate of heat transfer by convection, \(h\) is the convection heat transfer coefficient, \(A\) is the surface area through which heat is being transferred, \(T_w\) is the temperature of the combustion gases (assumed equal to the furnace wall temperature), and \(T\) is the temperature of the steel strip. By adjusting parameters like the convection coefficient \(h\), you can affect how rapidly heat is transferred to the material, which is essential when calculating the time and temperature profile for the annealing process.
Radiation Heat Transfer
In addition to convection, radiation heat transfer is a prominent player in the annealing process. Radiation differs from convection in that it doesn't require a medium to transfer heat; it occurs through electromagnetic waves. All objects emit radiation, and the amount depends on their temperature and emissivity.

The radiation heat transfer rate can be represented by the equation:
\(q_r = \varepsilon \times A \times \sigma \times (T_w^4 - T^4)\).

In this formula, \(q_r\) is the heat transfer rate due to radiation, \(\varepsilon\) is the emissivity of the strip's surface, and \(\sigma\) is the Stefan-Boltzmann constant, a fundamental parameter in the equation of radiant heat transfer. \(T_w\) and \(T\) are as previously defined. This form of heat transfer becomes particularly significant at higher temperatures. Since heat radiates from the furnace walls, which are at a high temperature, understanding radiation's contribution is crucial for predicting the heating rate and designing the annealing process effectively.
Energy Balance in Heat Transfer
The principle of energy balance is at the core of the entire heating process during annealing. It states that the energy flowing into a system minus the energy flowing out, plus the energy being generated within the system, equals the change in energy stored in the system.

Applied to our steel strip, the differential energy balance equation, derived from integrating the total heat transfer rate over time, is important for understanding how the strip's temperature changes as it moves through the furnace:
\(\frac{dq_{total}}{dt} = m \times c_p \times \frac{dT}{dt}\).

This equation equates the rate of heat transfer (\(dq_{total}\)) to the rate of change in energy stored in the strip, defined by its mass \(m\), specific heat \(c_p\), and the rate of change of temperature \(\frac{dT}{dt}\). Through this balance, we calculate the time required for the steel strip to reach the desired temperature. This calculation helps in optimizing the annealing process by adjusting the furnace length and controlling the time the strip spends within the furnace.
Heat Capacity
The heat capacity of a substance is a measure of the amount of heat energy required to raise the temperature of a given mass of the substance by a certain amount. In the case of the annealing process, the heat capacity plays a significant role in determining how the temperature of the steel strip changes over time.

To find the specific heat required, we use the equation:
\(m = \rho \times \delta \times A\)
,where \(m\) is the mass of the strip, \(\rho\) is the density, \(\delta\) is the thickness, and \(A\) is the cross-sectional area. Once we know the mass, we can quantify the energy involved in heating the strip with the equation:
\(\Delta E = m \times c_p \times (T_f - T_i)\)
.Here \(\Delta E\) is the change in energy or the energy absorbed by the strip, \(c_p\) is the specific heat capacity, and \(T_f\) and \(T_i\) are the final and initial temperatures. Through this understanding of heat capacity, we can effectively control the heating process to achieve the desired metallurgical properties in the steel strip after annealing.

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Most popular questions from this chapter

A metal sphere of diameter \(D\), which is at a uniform temperature \(T_{i}\), is suddenly removed from a furnace and suspended from a fine wire in a large room with air at a uniform temperature \(T_{\infty}\) and the surrounding walls at a temperature \(T_{\text {sur }}\) (a) Neglecting heat transfer by radiation, obtain an expression for the time required to cool the sphere to some temperature \(T\). (b) Neglecting heat transfer by convection, obtain an expression for the time required to cool the sphere to the temperature \(T\). (c) How would you go about determining the time required for the sphere to cool to the temperature \(T\) if both convection and radiation are of the same order of magnitude? (d) Consider an anodized aluminum sphere ( \(\varepsilon=0.75\) ) \(50 \mathrm{~mm}\) in diameter, which is at an initial temperature of \(T_{i}=800 \mathrm{~K}\). Both the air and surroundings are at \(300 \mathrm{~K}\), and the convection coefficient is \(10 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). For the conditions of parts (a), (b), and (c), determine the time required for the sphere to cool to \(400 \mathrm{~K}\). Plot the corresponding temperature histories. Repeat the calculations for a polished aluminum sphere ( \(\varepsilon=0.1)\).

A support rod \(\left(k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \alpha=4.0 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\right)\) of diameter \(D=15 \mathrm{~mm}\) and length \(L=100 \mathrm{~mm}\) spans a channel whose walls are maintained at a temperature of \(T_{b}=300 \mathrm{~K}\). Suddenly, the rod is exposed to a cross flow of hot gases for which \(T_{\infty}=600 \mathrm{~K}\) and \(h=75 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The channel walls are cooled and remain at \(300 \mathrm{~K}\). (a) Using an appropriate numerical technique, determine the thermal response of the rod to the convective heating. Plot the midspan temperature as a function of elapsed time. Using an appropriate analytical model of the rod, determine the steadystate temperature distribution, and compare the result with that obtained numerically for very long elapsed times. (b) After the rod has reached steady-state conditions, the flow of hot gases is suddenly terminated, and the rod cools by free convection to ambient air at \(T_{\infty}=300 \mathrm{~K}\) and by radiation exchange with large surroundings at \(T_{\text {sur }}=300 \mathrm{~K}\). The free convection coefficient can be expressed as \(h\left(\mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\right)=C\) \(\Delta T^{n}\), where \(C=4.4 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}^{1.188}\) and \(n=0.188\). The emissivity of the rod is \(0.5\). Determine the subsequent thermal response of the rod. Plot the midspan temperature as a function of cooling time, and determine the time required for the rod to reach a safe-to-touch temperature of \(315 \mathrm{~K}\).

In a manufacturing process, long rods of different diameters are at a uniform temperature of \(400^{\circ} \mathrm{C}\) in a curing oven, from which they are removed and cooled by forced convection in air at \(25^{\circ} \mathrm{C}\). One of the line operators has observed that it takes \(280 \mathrm{~s}\) for a \(40-\mathrm{mm}\) diameter rod to cool to a safe-to-handle temperature of \(60^{\circ} \mathrm{C}\). For an equivalent convection coefficient, how long will it take for an 80 -mm-diameter rod to cool to the same temperature? The thermophysical properties of the rod are \(\rho=2500 \mathrm{~kg} / \mathrm{m}^{3}, c=900 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), and \(k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). Comment on your result. Did you anticipate this outcome?

The objective of this problem is to develop thermal models for estimating the steady-state temperature and the transient temperature history of the electrical transformer shown. The external transformer geometry is approximately cubical, with a length of \(32 \mathrm{~mm}\) to a side. The combined mass of the iron and copper in the transformer is \(0.28 \mathrm{~kg}\), and its weighted-average specific heat is \(400 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\). The transformer dissipates \(4.0 \mathrm{~W}\) and is operating in ambient air at \(T_{\infty}=20^{\circ} \mathrm{C}\), with a convection coefficient of \(10 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). List and justify the assumptions made in your analysis, and discuss limitations of the models. (a) Beginning with a properly defined control volume, develop a model for estimating the steady-state temperature of the transformer, \(T(\infty)\). Evaluate \(T(\infty)\) for the prescribed operating conditions. (b) Develop a model for estimating the thermal response (temperature history) of the transformer if it is initially at a temperature of \(T_{i}=T_{\infty}\) and power is suddenly applied. Determine the time required for the transformer to come within \(5^{\circ} \mathrm{C}\) of its steady-state operating temperature.

Derive the explicit finite-difference equation for an interior node for three- dimensional transient conduction. Also determine the stability criterion. Assume constant properties and equal grid spacing in all three directions.

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