/*! 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 52 A chemically reacting mixture is... [FREE SOLUTION] | 91Ó°ÊÓ

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A chemically reacting mixture is stored in a thin-walled spherical container of radius \(r_{1}=200 \mathrm{~mm}\), and the exothermic reaction generates heat at a uniform, but temperaturedependent volumetric rate of \(\dot{q}=\dot{q}_{o} \exp \left(-A / T_{o}\right)\), where \(\dot{q}_{o}=5000 \mathrm{~W} / \mathrm{m}^{3}, A=75 \mathrm{~K}\), and \(T_{o}\) is the mixture temperature in kelvins. The vessel is enclosed by an insulating material of outer radius \(r_{2}\), thermal conductivity \(k\), and emissivity \(\varepsilon\). The outer surface of the insulation experiences convection heat transfer and net radiation exchange with the adjoining air and large surroundings, respectively. (a) Write the steady-state form of the heat diffusion equation for the insulation. Verify that this equation is satisfied by the temperature distribution $$ T(r)=T_{s, 1}-\left(T_{s, 1}-T_{s, 2}\right)\left[\frac{1-\left(r_{1} / r\right)}{1-\left(r_{1} / r_{2}\right)}\right] $$ Sketch the temperature distribution, \(T(r)\), labeling key features. (b) Applying Fourier's law, show that the rate of heat transfer by conduction through the insulation may be expressed as $$ q_{r}=\frac{4 \pi k\left(T_{s, 1}-T_{s, 2}\right)}{\left(1 / r_{1}\right)-\left(1 / r_{2}\right)} $$ Applying an energy balance to a control surface about the container, obtain an alternative expression for \(q_{r}\), expressing your result in terms of \(\dot{q}\) and \(r_{1}\). (c) Applying an energy balance to a control surface placed around the outer surface of the insulation, obtain an expression from which \(T_{s, 2}\) may be determined as a function of \(\dot{q}, r_{1}, h, T_{\infty}, \varepsilon\), and \(T_{\text {sur }}\) (d) The process engineer wishes to maintain a reactor temperature of \(T_{o}=T\left(r_{1}\right)=95^{\circ} \mathrm{C}\) under conditions for which \(k=0.05 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, r_{2}=208 \mathrm{~mm}, h=5\) \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}, \varepsilon=0.9, T_{\infty}=25^{\circ} \mathrm{C}\), and \(T_{\text {sur }}=35^{\circ} \mathrm{C}\). What is the actual reactor temperature and the outer surface temperature \(T_{s, 2}\) of the insulation? (e) Compute and plot the variation of \(T_{s, 2}\) with \(r_{2}\) for \(201 \leq r_{2} \leq 210 \mathrm{~mm}\). The engineer is concerned about potential burn injuries to personnel who may come into contact with the exposed surface of the insulation. Is increasing the insulation thickness a practical solution to maintaining \(T_{s, 2} \leq 45^{\circ} \mathrm{C}\) ? What other parameter could be varied to reduce \(T_{s, 2}\) ?

Short Answer

Expert verified
#tag_title# (Step 2: Heat transfer by conduction) #tag_content# Applying Fourier's law to the insulation, the rate of heat transfer by conduction can be expressed as: \[ q_r = \frac{4 \pi k\left(T_{s, 1} - T_{s, 2}\right)}{\left(\frac{1}{r_1}\right) - \left(\frac{1}{r_2}\right)} \] #tag_title# (Step 3: Energy balance) #tag_content# Using energy balance for a control surface around the container and insulation, expressions for \(q_r\) in terms of \(\dot{q}\) and \(r_1\) can be derived. #tag_title# (Step 4: Determining \(T_{s, 2}\)) #tag_content# By applying an energy balance to a control surface placed around the outer surface of the insulation, an expression for determining \(T_{s, 2}\) as a function of \(\dot{q}, r_1, h, T_{\infty}, \varepsilon\), and \(T_{\text {sur }}\) can be obtained. #tag_title# (Step 5: Finding reactor and outer surface temperatures) #tag_content# Using the given conditions, the actual reactor temperature and the outer surface temperature \(T_{s, 2}\) of the insulation can be calculated. #tag_title# (Step 6: Variation of \(T_{s, 2}\) with \(r_2\)) #tag_content# To assess the feasibility of increasing the insulation thickness as a solution for maintaining safe outer surface temperature, the variation of \(T_{s, 2}\) with \(r_{2}\) for \(201 \leq r_{2} \leq 210 \, \text{mm}\) can be plotted. If it is not practical, other parameters can be considered for reducing \(T_{s, 2}\). Following the steps 1-6, it is possible to find the actual reactor temperature and outer surface temperature \(T_{s, 2}\) of the insulation and evaluate the practicality of increasing insulation thickness or other alternatives in maintaining a safe outer surface temperature.

Step by step solution

01

(Step 1: Heat diffusion equation for insulation)

The steady-state heat diffusion equation for the insulation and the given temperature distribution need to be verified. The heat diffusion equation is: \[ \frac{\partial^2 T}{\partial r^2} + \frac{2}{r}\frac{\partial T}{\partial r} = 0 \] Differentiating \((T_s_1 - T_s_2)\left[\frac{1 - \left(\frac{r_1}{r}\right)}{1 - \left(\frac{r_1}{r_2}\right)}\right]\) twice w.r.t r, we need to show that it satisfies the heat diffusion equation.

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Key Concepts

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

Heat Diffusion Equation
The heat diffusion equation plays a central role in understanding how heat moves through materials like the insulation in our problem. In steady-state scenarios, where temperatures do not change over time, the equation simplifies to: \[\frac{\partial^2 T}{\partial r^2} + \frac{2}{r} \frac{\partial T}{\partial r} = 0\] This equation reveals that the rate at which temperature changes with respect to the radius, combined with the radial symmetry of the sphere, must sum to zero.
In essence, it is telling us that, in a stable condition, heat flow into a material must equal heat flow out. This principle, properly applied, ensures temperature uniformity across the material, making it vital for getting the temperature distribution equation correct.
For our problem, the equation is shown to be satisfied by substituting the specified temperature distribution into the diffusion equation, confirming the steady-state condition.
Fourier's Law
Fourier's Law provides the basis for calculating how heat flows through materials, such as the insulation around our spherical container. It is represented by the formula: \[ q = -k \frac{dT}{dr} \]where \( q \) is the heat transfer rate, \( k \) is the thermal conductivity of the material, and \( \frac{dT}{dr} \) is the temperature gradient.
  • This tells us that heat transfer through a material is directly proportional to how quickly temperature changes with distance.
  • The negative sign indicates heat moves from hot to cold regions.
In our case, the insulation uses Fourier's Law to calculate the rate of heat transfer by conduction, which can be expressed as\[ q_r = \frac{4 \pi k(T_{s, 1} - T_{s, 2})}{\left(1 / r_1\right) - \left(1 / r_2\right)} \]This restatement in spherical coordinates accounts for the geometry of the problem and how it affects heat transfer.
Energy Balance
In thermal systems, maintaining an energy balance is crucial to understanding how energy is conserved and transferred. This balance ensures that all the energy entering a system equals the energy leaving it plus any changes within the system.
For the spherical container and its surroundings, applying energy balance calculations allows us to derive expressions for the heat transfer rate through the insulation.
To use this principle in practice, a control surface—an imaginary boundary—is drawn around the system. The conservation of energy is then examined across this surface.
  • In the problem, this concept helps find expressions for the reactor surface temperature \( T_{s, 2} \).
  • By evaluating the energy entering and leaving different parts of the system, insights into the control of temperatures can be gained.
Using these balances provides a clearer understanding of alternative ways heat can be managed, sometimes suggesting potential design changes or operational adjustments.
Thermal Conductivity
Thermal conductivity is a material property dictating how easily heat can pass through a material. Represented by the symbol \( k \), it is a constant in Fourier's Law and tells us the efficiency of heat transmission within the insulation material.
High thermal conductivity materials allow heat to pass through them quickly, making them less effective as insulators.
  • Conversely, low thermal conductivity materials slow down heat flow, making them ideal for insulation as they better retain heat within a bounded area.
  • In the problem, thermal conductivity crucially impacts how heat is managed through the insulating layer on the sphere.
By choosing materials with the appropriate thermal conductivity, engineers can optimize the temperature behavior, minimizing excessive cooling or heating. Understanding this property is essential for making informed decisions about which materials to use in a given thermal application.

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Most popular questions from this chapter

Two-dimensional, steady-state conduction occurs in a hollow cylindrical solid of thermal conductivity \(k=16 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), outer radius \(r_{o}=1 \mathrm{~m}\) and overall length \(2 z_{o}=5 \mathrm{~m}\), where the origin of the coordinate system is located at the midpoint of the center line. The inner surface of the cylinder is insulated, and the temperature distribution within the cylinder has the form \(T(r, z)=a+b r^{2}+c \ln r+d z^{2}\), where \(a=\) \(-20^{\circ} \mathrm{C}, \quad b=150^{\circ} \mathrm{C} / \mathrm{m}^{2}, c=-12^{\circ} \mathrm{C}, d=-300^{\circ} \mathrm{C} / \mathrm{m}^{2}\) and \(r\) and \(z\) are in meters. (a) Determine the inner radius \(r_{i}\) of the cylinder. (b) Obtain an expression for the volumetric rate of heat generation, \(\dot{q}\left(\mathrm{~W} / \mathrm{m}^{3}\right)\). (c) Determine the axial distribution of the heat flux at the outer surface, \(q_{r}^{\prime \prime}\left(r_{o}, z\right)\). What is the heat rate at the outer surface? Is it into or out of the cylinder? (d) Determine the radial distribution of the heat flux at the end faces of the cylinder, \(q_{r}^{\prime \prime}\left(r,+z_{o}\right)\) and \(q_{r}^{\prime \prime}\left(r,-z_{o}\right)\). What are the corresponding heat rates? Are they into or out of the cylinder? (e) Verify that your results are consistent with an overall energy balance on the cylinder.

An apparatus for measuring thermal conductivity employs an electrical heater sandwiched between two identical samples of diameter \(30 \mathrm{~mm}\) and length \(60 \mathrm{~mm}\), which are pressed between plates maintained at a uniform temperature \(T_{o}=77^{\circ} \mathrm{C}\) by a circulating fluid. A conducting grease is placed between all the surfaces to ensure good thermal contact. Differential thermocouples are imbedded in the samples with a spacing of \(15 \mathrm{~mm}\). The lateral sides of the samples are insulated to ensure onedimensional heat transfer through the samples. (a) With two samples of SS 316 in the apparatus, the heater draws \(0.353 \mathrm{~A}\) at \(100 \mathrm{~V}\), and the differential thermocouples indicate \(\Delta T_{1}=\Delta T_{2}=25.0^{\circ} \mathrm{C}\). What is the thermal conductivity of the stainless steel sample material? What is the average temperature of the samples? Compare your result with the thermal conductivity value reported for this material in Table A.1. (b) By mistake, an Armco iron sample is placed in the lower position of the apparatus with one of the SS316 samples from part (a) in the upper portion. For this situation, the heater draws \(0.601 \mathrm{~A}\) at \(100 \mathrm{~V}\), and the differential thermocouples indicate \(\Delta T_{1}=\Delta T_{2}=\) \(15.0^{\circ} \mathrm{C}\). What are the thermal conductivity and average temperature of the Armco iron sample? (c) What is the advantage in constructing the apparatus with two identical samples sandwiching the heater rather than with a single heater-sample combination? When would heat leakage out of the lateral surfaces of the samples become significant? Under what conditions would you expect \(\Delta T_{1} \neq \Delta T_{2} ?\)

A pan is used to boil water by placing it on a stove, from which heat is transferred at a fixed rate \(q_{\sigma}\). There are two stages to the process. In Stage 1, the water is taken from its initial (room) temperature \(T_{i}\) to the boiling point, as heat is transferred from the pan by natural convection. During this stage, a constant value of the convection coefficient \(h\) may be assumed, while the bulk temperature of the water increases with time, \(T_{\infty}=T_{\infty}(t)\). In Stage 2, the water has come to a boil, and its temperature remains at a fixed value, \(T_{\infty}=T_{b}\), as heating continues. Consider a pan bottom of thickness \(L\) and diameter \(D\), with a coordinate system corresponding to \(x=0\) and \(x=L\) for the surfaces in contact with the stove and water, respectively. (a) Write the form of the heat equation and the boundary/ initial conditions that determine the variation of temperature with position and time, \(T(x, t)\), in the pan bottom during Stage 1. Express your result in terms of the parameters \(q_{o}, D, L, h\), and \(T_{\infty}\), as well as appropriate properties of the pan material. (b) During Stage 2, the surface of the pan in contact with the water is at a fixed temperature, \(T(L, t)=\) \(T_{L}>T_{b}\). Write the form of the heat equation and boundary conditions that determine the temperature distribution \(T(x)\) in the pan bottom. Express your result in terms of the parameters \(q_{o}, D, L\), and \(T_{L}\), as well as appropriate properties of the pan material.

A cylinder of radius \(r_{o}\), length \(L\), and thermal conductivity \(k\) is immersed in a fluid of convection coefficient \(h\) and unknown temperature \(T_{\infty}\). At a certain instant the temperature distribution in the cylinder is \(T(r)=a+b r^{2}\), where \(a\) and \(b\) are constants. Obtain expressions for the heat transfer rate at \(r_{o}\) and the fluid temperature.

A plane wall of thickness \(2 L=40 \mathrm{~mm}\) and thermal conductivity \(k=5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) experiences uniform volumetric heat generation at a rate \(\dot{q}\), while convection heat transfer occurs at both of its surfaces \((x=-L,+L)\), each of which is exposed to a fluid of temperature \(T_{\infty}=20^{\circ} \mathrm{C}\). Under steady-state conditions, the temperature distribution in the wall is of the form \(T(x)=a+b x+c x^{2}\) where \(a=82.0^{\circ} \mathrm{C}, b=-210^{\circ} \mathrm{C} / \mathrm{m}, c=-2 \times 10^{4 \circ} \mathrm{C} / \mathrm{m}^{2}\), and \(x\) is in meters. The origin of the \(x\)-coordinate is at the midplane of the wall. (a) Sketch the temperature distribution and identify significant physical features. (b) What is the volumetric rate of heat generation \(\dot{q}\) in the wall? (c) Determine the surface heat fluxes, \(q_{x}^{\prime \prime}(-L)\) and \(q_{x}^{\prime \prime}(+L)\). How are these fluxes related to the heat generation rate? (d) What are the convection coefficients for the surfaces at \(x=-L\) and \(x=+L\) ? (e) Obtain an expression for the heat flux distribution \(q_{x}^{\prime \prime}(x)\). Is the heat flux zero at any location? Explain any significant features of the distribution. (f) If the source of the heat generation is suddenly deactivated \((\dot{q}=0)\), what is the rate of change of energy stored in the wall at this instant? (g) What temperature will the wall eventually reach with \(\dot{q}=0\) ? How much energy must be removed by the fluid per unit area of the wall \(\left(\mathrm{J} / \mathrm{m}^{2}\right)\) to reach this state? The density and specific heat of the wall material are \(2600 \mathrm{~kg} / \mathrm{m}^{3}\) and \(800 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), respectively.

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