/*! 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 An experimental nuclear core sim... [FREE SOLUTION] | 91影视

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An experimental nuclear core simulation apparatus consists of a long thin- walled metallic tube of diameter \(D\) and length \(L\), which is electrically heated to produce the sinusoidal heat flux distribution $$ q_{s}^{\prime \prime}(x)=q_{o}^{\prime \prime} \sin \left(\frac{\pi x}{L}\right) $$ where \(x\) is the distance measured from the tube inlet. Fluid at an inlet temperature \(T_{m, i}\) flows through the tube at a rate of \(\dot{m}\). Assuming the flow is turbulent and fully developed over the entire length of the tube, develop expressions for: (a) the total rate of heat transfer, \(q\), from the tube to the fluid; (b) the fluid outlet temperature, \(T_{m, o} ;\) (c) the axial distribution of the wall temperature, \(T_{s}(x)\); and (d) the magnitude and position of the highest wall temperature. (e) Consider a \(40-\mathrm{mm}\)-diameter tube of \(4-\mathrm{m}\) length with a sinusoidal heat flux distribution for which \(q_{o}^{\prime \prime}=10,000 \mathrm{~W} / \mathrm{m}^{2}\). Fluid passing through the tube has a flow rate of \(0.025 \mathrm{~kg} / \mathrm{s}\), a specific heat of \(4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), an entrance temperature of \(25^{\circ} \mathrm{C}\), and a convection coefficient of \(1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Plot the mean fluid and surface temperatures as a function of distance along the tube. Identify important features of the distributions. Explore the effect of \(\pm 25 \%\) changes in the convection coefficient and the heat flux on the distributions.

Short Answer

Expert verified
In summary, we have derived expressions for the total rate of heat transfer, fluid outlet temperature, axial distribution of the wall temperature, and the magnitude and position of the highest wall temperature in the given experimental nuclear core simulation apparatus. The total rate of heat transfer is given by \(q = q_o'' A \frac{2L}{\pi}\), the fluid outlet temperature is given by \(T_{m, o} = T_{m, i} + \frac{q_o'' A \frac{2L}{\pi}}{\dot{m} C_p}\), the axial distribution of the wall temperature is given by \(T_s(x) = T_{m, x} + \frac{q_o'' \sin \left(\frac{\pi x}{L}\right)}{h}\), and the highest wall temperature occurs at \(x = \frac{L}{2}\) with a magnitude of \(T_{s, max} = T_{m, \frac{L}{2}} + \frac{q_o''}{h}\). Given the specific data for the tube, fluid, and convection coefficient expressions, we can use numerical or graphical software to plot the mean fluid and surface temperatures and analyze the effect of varying the convection coefficient and the heat flux on the distributions.

Step by step solution

01

a) Total rate of heat transfer

The formula for the total rate of heat transfer can be derived by substituting the given heat flux distribution expression into the integral above: $$ q = \int_0^L q_o'' \sin \left( \frac{\pi x}{L} \right) A dx = q_o'' A \int_0^L \sin \left( \frac{\pi x}{L} \right) dx $$ Now, we solve the integral: $$ q = q_o'' A \left[ -\frac{L}{\pi} \cos \left( \frac{\pi x}{L} \right) \right]_0^L = -q_o'' A \frac{L}{\pi} \left[\cos \left( \pi \right) - \cos \left( 0 \right) \right] = q_o'' A \frac{2L}{\pi} $$ So the total rate of heat transfer from the tube to the fluid is: $$ q = q_o'' A \frac{2L}{\pi} $$
02

b) Fluid outlet temperature

To find the fluid outlet temperature, we can use the energy balance equation: $$ q = \dot{m} C_p (T_{m, o} - T_{m, i}) $$ Rearranging for the fluid outlet temperature, we have: $$ T_{m, o} = T_{m, i} + \frac{q}{\dot{m} C_p} = T_{m, i} + \frac{q_o'' A \frac{2L}{\pi}}{\dot{m} C_p} $$
03

c) Axial distribution of the wall temperature

The heat transfer equation for convection is: $$ q_s''(x) = h [T_s(x) - T_{m, x}] $$ Solving for the wall temperature, we get: $$ T_s(x) = T_{m, x} + \frac{q_s''(x)}{h} $$ We substitude the given heat flux distribution, so: $$ T_s(x) = T_{m, x} + \frac{q_o'' \sin \left(\frac{\pi x}{L}\right)}{h} $$
04

d) Magnitude and position of the highest wall temperature

The highest wall temperature occurs when \(q_s''\) is at its maximum value. The maximum value of the sinusoidal term \(\sin \left(\frac{\pi x}{L}\right)\) is 1, so the position of the highest wall temperature is when: $$ x = \frac{L}{2} $$ Substituting this value of \(x\) into the expression for \(T_s(x)\), we get: $$ T_{s, max} = T_{m, \frac{L}{2}} + \frac{q_o''}{h} $$
05

e) Mean fluid and surface temperatures

Given the specific data for the tube, fluid, and convection coefficient expressions, we can plot the mean fluid and surface temperatures as a function of distance along the tube by evaluating the expression for \(T_s(x)\) using the given data and varying the convection coefficient and heat flux as indicated. This task is best done using a numerical or graphical software package, such as MATLAB, to generate the desired plots and analyze the effect of varying the convection coefficient and the heat flux on the distributions.

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Key Concepts

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

Heat Transfer Rate
Understanding the heat transfer rate in a nuclear core simulation is crucial to maintaining safety and efficiency in nuclear reactors. In our exercise, the heat transfer rate refers to the amount of thermal energy moved from the metallic tube's wall to the fluid flowing through it. The rate of heat transfer, denoted by the symbol q, is found by integrating the given sinusoidal heat flux distribution qs''(x) over the tube's surface area A and its length L.

Mathematically, this is expressed and solved as q = qo'' A (2L/蟺), where qo'' is the peak heat flux. It is key to note that the total heat transfer is directly proportional to both the surface area and the length of the tube, implying the larger these factors, the greater the potential for heat transfer to occur.
Fluid Outlet Temperature
The fluid outlet temperature, labeled Tm,o, is an important metric as it indicates how much the fluid has heated up after traversing the tube's length. To find Tm,o, the exercise applies an energy balance that equates the heat transfer to the fluid's thermal energy change. The formula derived is Tm,o = Tm,i + (q/峁丆p), which takes into account the mass flow rate , the specific heat of the fluid Cp, and the inlet temperature Tm,i.

This relationship implies that the outlet temperature is influenced by the characteristics of the fluid, the heat absorbed, and the initial temperature. Therefore, by adjusting the flow rate or the fluid's specific heat, the thermal performance of the system can be managed.
Wall Temperature Distribution
In a nuclear reactor core simulation, understanding the wall temperature distribution is vital for predicting the thermal stresses and potential for material failure. According to our problem, the wall temperature Ts(x) varies along the length of the tube and depends on the local fluid temperature and the heat flux. Using the heat transfer equation for convection, Ts(x) = Tm,x + (qs''(x)/h), we can predict how temperature changes from the inlet to the outlet.

The maximum wall temperature, crucial for safety analysis, occurs at the position where the heat flux's sinusoidal distribution reaches its peak. Our exercise establishes that this happens at the midpoint of the tube's length, ensuring that the structural integrity of the tube remains uncompromised under these conditions. This information is essential for designing reactor components resilient to thermal fluctuations.
Thermal Analysis of Nuclear Reactors
The thermal analysis of nuclear reactors, like the simulation presented, is a sophisticated process that involves predicting how temperatures will vary within the reactor. It's not only about determining individual parameters, but also understanding how they interrelate and affect the reactor's performance and safety.

For instance, altering the convection coefficient or the heat flux can have significant effects on fluid and surface temperature distributions. The exercise suggests exploring the impact of a 卤25% change in these values, which is a practical approach to study the behavior under different conditions. Through the use of numerical or graphical software, detailed plots can be generated to visually articulate these effects, providing insight necessary for reactor design and operation.

In conclusion, thermal analysis integrates various concepts like heat transfer rate, fluid mechanics, and thermal properties, with the end goal being to maintain the integrity and safety of nuclear reactors during operation.

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Most popular questions from this chapter

Engine oil is heated by flowing through a circular tube of diameter \(D=50 \mathrm{~mm}\) and length \(L=25 \mathrm{~m}\) and whose surface is maintained at \(150^{\circ} \mathrm{C}\). (a) If the flow rate and inlet temperature of the oil are \(0.5 \mathrm{~kg} / \mathrm{s}\) and \(20^{\circ} \mathrm{C}\), what is the outlet temperature \(T_{m, o}\) ? What is the total heat transfer rate \(q\) for the tube? (b) For flow rates in the range \(0.5 \leq \dot{m} \leq 2.0 \mathrm{~kg} / \mathrm{s}\), compute and plot the variations of \(T_{m, o}\) and \(q\) with \(\dot{m}\). For what flow rate(s) are \(q\) and \(T_{m, \rho}\) maximized? Explain your results.

Water flowing at \(2 \mathrm{~kg} / \mathrm{s}\) through a \(40-\mathrm{mm}\)-diameter tube is to be heated from 25 to \(75^{\circ} \mathrm{C}\) by maintaining the tube surface temperature at \(100^{\circ} \mathrm{C}\). (a) What is the required tube length for these conditions? (b) To design a water heating system, we wish to consider using tube diameters in the range from 30 to \(50 \mathrm{~mm}\). What are the required tube lengths for water flow rates of 1,2 , and \(3 \mathrm{~kg} / \mathrm{s}\) ? Represent this design information graphically. (c) Plot the pressure gradient as a function of tube diameter for the three flow rates. Assume the tube wall is smooth.

Water at \(\dot{m}=0.02 \mathrm{~kg} / \mathrm{s}\) and \(T_{m, i}=20^{\circ} \mathrm{C}\) enters an annular region formed by an inner tube of diameter \(D_{i}=25 \mathrm{~mm}\) and an outer tube of diameter \(D_{o}=100 \mathrm{~mm}\). Saturated steam flows through the inner tube, maintaining its surface at a uniform temperature of \(T_{s, i}=100^{\circ} \mathrm{C}\), while the outer surface of the outer tube is well insulated. If fully developed conditions may be assumed throughout the annulus, how long must the system be to provide an outlet water temperature of \(75^{\circ} \mathrm{C}\) ? What is the heat flux from the inner tube at the outlet?

8.105 The mold used in an injection molding process consists of a top half and a bottom half. Each half is \(60 \mathrm{~mm} \times 60 \mathrm{~mm} \times 20 \mathrm{~mm}\) and is constructed of metal \(\left(\rho=7800 \mathrm{~kg} / \mathrm{m}^{3}, \quad c=450 \mathrm{~J} / \mathrm{kg}+\mathrm{K}\right)\). The cold mold \(\left(100^{\circ} \mathrm{C}\right)\) is to be heated to \(200^{\circ} \mathrm{C}\) with pressurized water (available at \(275^{\circ} \mathrm{C}\) and a total flow rate of \(0.02 \mathrm{~kg} / \mathrm{s}\) ) prior to injecting the thermoplastic material. The injection takes only a fraction of a second, and the hot mold \(\left(200^{\circ} \mathrm{C}\right)\) is subsequently cooled with cold water (available at \(25^{\circ} \mathrm{C}\) and a total flow rate of \(0.02 \mathrm{~kg} / \mathrm{s})\) prior to ejecting the molded part. After part ejection, which also takes a fraction of a second, the process is repeated. (a) In conventional mold design, straight cooling (heating) passages are bored through the mold in a location where the passages will not interfere with the molded part. Determine the initial heating rate and the initial cooling rate of the mold when five 5 -mm-diameter, 60-mm-long passages are bored in each half of the mold (10 passages total). The velocity distribution of the water is fully developed at the entrance of each passage in the hot (or cold) mold. (b) New additive manufacturing processes, known as selective freeform fabrication, or \(S F F\), are used to construct molds that are configured with conformal cooling passages. Consider the same mold as before, but now a 5 -mm- diameter, coiled, conformal cooling passage is designed within each half of the SFF-manufactured mold. Each of the two coiled passages has \(N=2\) turns. The coiled passage does not interfere with the molded part. The conformal channels have a coil diameter \(C=50 \mathrm{~mm}\). The total water flow remains the same as in part (a) \((0.01 \mathrm{~kg} / \mathrm{s}\) per coil). Determine the initial heating rate and the initial cooling rate of the mold. (c) Compare the surface areas of the conventional and conformal cooling passages. Compare the rate at which the mold temperature changes for molds configured with the conventional and conformal heating and cooling passages. Which cooling passage, conventional or conformal, will enable production of more parts per day? Neglect the presence of the thermoplastic material.

Air at \(1 \mathrm{~atm}\) and \(285 \mathrm{~K}\) enters a 2 -m-long rectangular duct with cross section \(75 \mathrm{~mm} \times 150 \mathrm{~mm}\). The duct is maintained at a constant surface temperature of \(400 \mathrm{~K}\), and the air mass flow rate is \(0.10 \mathrm{~kg} / \mathrm{s}\). Determine the heat transfer rate from the duct to the air and the air outlet temperature.

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