/*! 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 123 In a thin-slab, continuous casti... [FREE SOLUTION] | 91Ó°ÊÓ

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In a thin-slab, continuous casting process, molten steel leaves a mold with a thin solid shell, and the molten material solidifies as the slab is quenched by water jets en route to a section of rollers. Once fully solidified, the slab continues to cool as it is brought to an acceptable handling temperature. It is this portion of the process that is of interest. Consider a 200-mm-thick solid slab of steel \(\left(\rho=7800 \mathrm{~kg} / \mathrm{m}^{3}, \quad c=700 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, \quad k=30 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\), initially at a uniform temperature of \(T_{i}=1400^{\circ} \mathrm{C}\). The slab is cooled at its top and bottom surfaces by water jets \(\left(T_{\infty}=50^{\circ} \mathrm{C}\right)\), which maintain an approximately uniform convection coefficient of \(h=5000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) at both surfaces. Using a finite-difference solution with a space increment of \(\Delta x=1 \mathrm{~mm}\), determine the time required to cool the surface of the slab to \(200^{\circ} \mathrm{C}\). What is the corresponding temperature at the midplane of the slab? If the slab moves at a speed of \(V=15 \mathrm{~mm} / \mathrm{s}\), what is the required length of the cooling section?

Short Answer

Expert verified
The time required to cool a 200-mm-thick steel slab's surface to 200°C can be calculated using an explicit finite-difference method for transient heat conduction. Initialize the temperature profile with the initial uniform temperature (1400°C), iterate and update the temperature profile at each time step, and stop when the surface temperature reaches or goes below 200°C. With the recorded time increment, find the midplane temperature from the central node of the finite-difference grid. The cooling section's required length can be calculated as \(Length = 15 \mathrm{~mm/s} \times Time\).

Step by step solution

01

Set up the finite-difference equations

To model transient heat conduction using an explicit finite-difference scheme, we use the energy equation: \(\frac{T'^{j + 1} - T^{j}}{\Delta t}= \alpha \frac{T'^{j - 1} - 2 T^{j} + T'^{j + 1}}{\Delta x^{2}}\) where \(T'^{j}\) represents the temperature at the node j, \(T^{j + 1}\) and \(T'^{j - 1}\) represent the temperatures at the neighboring nodes, \(\Delta t\) is the time step, \(\Delta x\) is the spatial step (given as 1 mm), and \(\alpha\) is the thermal diffusivity. We will need to determine the thermal diffusivity using the provided material properties: \(\alpha = \frac{k}{\rho c} = \frac{30 \mathrm{~W/m\cdot K}}{7800 \mathrm{~kg/m^3} \cdot 700 \mathrm{~J/kg\cdot K}} = 5.5 \times 10^{-6} \mathrm{~m^2/s}\)
02

Initialize the temperature profile

We start with an initial uniform temperature of 1400°C across the slab. For each node in our finite-difference grid, the initial temperature \(T^{0}\) is set to 1400°C.
03

Iterate to find the temperature profile at each time step

Using the explicit finite difference method, we can calculate the temperatures at each node for the subsequent times. Iterate through the time steps until the condition of the surface temperature reaching 200°C is met.
04

Check if the surface temperature has reached 200°C

Once the temperature at the surface (first node) reaches 200°C or below, stop iterating. Record the time increment at this point to calculate the time required to cool the slab.
05

Calculate midplane temperature and cooling section length

Once the surface temperature has reached 200°C, we can find the temperature at the midplane and compute the required length of the cooling section. - The midplane temperature can be calculated from the temperature at the central node of our finite-difference grid. - The required cooling section length can be found using the slab speed and the recorded time increment: \(Length = V \times Time = 15 \mathrm{~mm/s} \times Time\) Finally, we obtain the time required to cool the slab to 200°C, the temperature at the midplane, and the required length of the cooling section.

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Key Concepts

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

Finite-Difference Solution
Understanding the finite-difference solution is crucial for modeling various engineering problems, including the cooling of a steel slab. This numerical method is applied to solve differential equations that describe physical phenomena, such as heat transfer, by approximating them using algebraic equations.

The method discretizes the continuous domain into a grid of nodes and iteratively solves the temperature at each node. A simple explicit finite-difference scheme, which is suitable for time-dependent problems, calculates the future temperature based on the current temperature and the temperatures of the neighboring nodes. This approach provides an approximation of the transient behavior of heat within the slab.

For an easier grasp of the finite-difference method, imagine the steel slab split into thin layers. Each layer's temperature at the next moment in time depends on its present temperature and the temperatures of the layers next to it. The calculations are made progressively, simulating how the slab cools over time until the surface reaches the desired temperature of 200°C.
Transient Heat Conduction
Transient heat conduction refers to the situation where temperature changes with time within a material. Unlike steady-state heat conduction, where the temperature at any point in the material does not change with time, transient analysis requires understanding how heat diffuses through the material over time and affects its temperature distribution.

In the case of the steel slab, when it is initially at a uniform high temperature and suddenly exposed to water jets, the temperature changes are not instantaneous throughout the slab. The outer surfaces cool down quicker than the inner layers, creating a temperature gradient. To successfully predict how long it takes for the surface to cool to 200°C, one must consider the material's properties such as thermal conductivity, density, and specific heat, which govern the rate of heat conduction. In layman's terms, think of transient heat conduction as watching a hot cup of coffee cool over time, where the temperature at each moment is influenced by the temperature from the moment before.
Convection Heat Transfer
Convection heat transfer is one of the main methods by which heat moves between a solid surface and a fluid. In the exercise, we deal with forced convection as water jets speed up the cooling process of the steel slab. The convection heat transfer's effectiveness is quantified by the convection coefficient 'h'. A higher value of 'h' represents more efficient heat removal from the surface.

The convection coefficient given for the cooling of the slab indicates how quickly the water jets can take heat away from the steel. This cooling rate is essential for determining how fast the surface temperature drops and, consequently, how long the cooling section needs to be to achieve the desired temperature.

To put it simply, imagine you're blowing on a spoonful of hot soup to cool it down; this is similar to how the water jets cool the slab. The 'h' value is like how effectively your blowing cools the soup, and it's essential for figuring out how long to blow on it before it’s cool enough to eat.

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Most popular questions from this chapter

Consider the fuel element of Example 5.11. Initially, the element is at a uniform temperature of \(250^{\circ} \mathrm{C}\) with no heat generation. Suddenly, the element is inserted into the reactor core, causing a uniform volumetric heat generation rate of \(\dot{q}=10^{8} \mathrm{~W} / \mathrm{m}^{3}\). The surfaces are convectively cooled with \(T_{\infty}=250^{\circ} \mathrm{C}\) and \(h=1100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Using the explicit method with a space increment of \(2 \mathrm{~mm}\), determine the temperature distribution \(1.5 \mathrm{~s}\) after the element is inserted into the core.

In a tempering process, glass plate, which is initially at a uniform temperature \(T_{i}\), is cooled by suddenly reducing the temperature of both surfaces to \(T_{s}\). The plate is \(20 \mathrm{~mm}\) thick, and the glass has a thermal diffusivity of \(6 \times 10^{-7} \mathrm{~m}^{2} / \mathrm{s}\). (a) How long will it take for the midplane temperature to achieve \(50 \%\) of its maximum possible temperature reduction? (b) If \(\left(T_{i}-T_{s}\right)=300^{\circ} \mathrm{C}\), what is the maximum temperature gradient in the glass at the time calculated in part (a)?

In Section \(5.2\) we noted that the value of the Biot number significantly influences the nature of the temperature distribution in a solid during a transient conduction process. Reinforce your understanding of this important concept by using the IHT model for one-dimensional transient conduction to determine radial temperature distributions in a 30 -mm-diameter, stainless steel rod \(\left(k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=8000 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=475 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\), as it is cooled from an initial uniform temperature of \(325^{\circ} \mathrm{C}\) by a fluid at \(25^{\circ} \mathrm{C}\). For the following values of the convection coefficient and the designated times, determine the radial temperature distribution: \(h=100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) \((t=0,100,500 \mathrm{~s}) ; h=1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}(t=0,10,50 \mathrm{~s})\); \(h=5000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}(t=0,1,5,25 \mathrm{~s})\). Prepare a separate graph for each convection coefficient, on which temperature is plotted as a function of dimensionless radius at the designated times.

The stability criterion for the explicit method requires that the coefficient of the \(T_{m}^{p}\) term of the one-dimensional, finite-difference equation be zero or positive. Consider the situation for which the temperatures at the two neighboring nodes \(\left(T_{\mathrm{m}-1}^{p}, T_{\mathrm{m}+1}^{p}\right)\) are \(100^{\circ} \mathrm{C}\) while the center node \(\left(T_{m}^{p}\right)\) is at \(50^{\circ} \mathrm{C}\). Show that for values of \(F o>\frac{1}{2}\) the finite-difference equation will predict a value of \(T_{m}^{p+1}\) that violates the second law of thermodynamics.

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.

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