/*! 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 86 An air heater may be fabricated ... [FREE SOLUTION] | 91Ó°ÊÓ

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An air heater may be fabricated by coiling Nichrome wire and passing air in cross flow over the wire. Consider a heater fabricated from wire of diameter \(D=\) \(1 \mathrm{~mm}\), electrical resistivity \(\rho_{e}=10^{-6} \Omega \cdot \mathrm{m}\), thermal conductivity \(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and emissivity \(\varepsilon=0.20\). The heater is designed to deliver air at a temperature of \(T_{\infty}=50^{\circ} \mathrm{C}\) under flow conditions that provide a convection coefficient of \(h=250 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) for the wire. The temperature of the housing that encloses the wire and through which the air flows is \(T_{\text {sur }}=50^{\circ} \mathrm{C}\). If the maximum allowable temperature of the wire is \(T_{\max }=1200^{\circ} \mathrm{C}\), what is the maximum allowable electric current \(I\) ? If the maximum available voltage is \(\Delta E=110 \mathrm{~V}\), what is the corresponding length \(L\) of wire that may be used in the heater and the power rating of the heater? Hint: In your solution, assume negligible temperature variations within the wire, but after obtaining the desired results, assess the validity of this assumption.

Short Answer

Expert verified
The maximum allowable electric current for the air heater is approximately \(13.81\,\text{A}\). The corresponding length of the Nichrome wire that may be used in the heater is about \(50\,\text{m}\), and the power rating of the heater is approximately \(1516.49\,\text{W}\).

Step by step solution

01

Find the maximum heat generated by the wire.

We need to find the electric power generated by the wire. By Ohm's law, we can write the power as: \[P_\text{e} = I^2 R\] Where \(I\) is the current and \(R\) is the resistance of the wire. Since our goal is to find the maximum allowable current, let's express the resistance \(R\) in terms of wire length \(L\) and resistivity \(\rho_e\), \[R = \frac{\rho_e L}{A} = \frac{\rho_e L}{\pi (D/2)^2}\] Now, substituting the resistance back to the power equation, we get: \[P_\text{e} = I^2 \frac{\rho_e L}{\pi(D/2)^2}\]
02

Find the heat dissipated by convection and radiation.

The heat dissipated by the wire can be broken into two components - convection and radiation. Find the heat transfer by convection: \[P_\text{c} = h A_c (T_\text{max} - T_\infty)\] Where \(A_c = \pi D L\) is the surface area for convection. Find the heat transfer by radiation: \[P_\text{r} = \varepsilon \sigma A_c (T_\text{max}^4 - T_\text{sur}^4)\] Where \(\sigma\) is the Stefan-Boltzmann constant, which equals \(5.67 \times 10^{-8}\, \text{W} / (\text{m}^2 \cdot \text{K}^4)\). Now, sum up these two components, since they both dissipate heat: \[P_\text{total} = P_\text{c} + P_\text{r} = h \pi D L (T_\text{max} - T_\infty) + \varepsilon \sigma \pi D L (T_\text{max}^4 - T_\text{sur}^4)\]
03

Equating the electrical power and total power heat dissipation to find the maximum current.

Since the electrical power generated by the wire should be equal to the total heat dissipated by convection and radiation, we can equate them: \[I^2 \frac{\rho_e L}{\pi (D/2)^2} = h \pi D L (T_\text{max} - T_\infty) + \varepsilon \sigma \pi D L (T_\text{max}^4 - T_\text{sur}^4)\] Simplify the equation and solve for the current \(I\): \[I = \sqrt{\frac{h \pi^2 D^3 (T_\text{max} - T_\infty) + \varepsilon \sigma \pi^2 D^3 (T_\text{max}^4 - T_\text{sur}^4)}{\rho_e}}\] Substitute the given values to find the maximum allowable current \(I\): \[I = \sqrt{\frac{250 \pi^2 (0.001)^3 (1200 - 50) + 0.20 (5.67 \times 10^{-8}) \pi^2 (0.001)^3 ((1200 + 273)^4 - (50 + 273)^4)}{10^{-6}}}\] \[I \approx 13.81\,\text{A}\] So, the maximum allowable electric current is about \(13.81\,\text{A}\).
04

Calculate the length of the Nichrome wire and the power rating of the heater.

Using Ohm's law, we can find the resistance of the wire: \[R = \frac{\Delta E}{I} = \frac{110\,\text{V}}{13.81\,\text{A}} \approx 7.96\,\Omega\] Calculate the length of the wire and substituting the given values: \[L = \frac{\pi (D/2)^2}{\rho_e} R\] \[L = \frac{\pi (0.001/2)^2}{10^{-6}} (7.96) \approx 50\,\text{m}\] Now, find the power rating of the heater: \[P_\text{total} = I^2 R \approx (13.81)^2 (7.96) \approx 1516.49\,\text{W}\] So, the corresponding length of the wire that may be used in the heater is around \(50\,\text{m}\) and the power rating of the heater is approximately \(1516.49\,\text{W}\).

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Key Concepts

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

Convection Heat Transfer
Convection is a mechanism of heat transfer where thermal energy is carried away by a fluid, such as air or water, which is in motion. Accompanying an exercise like the one provided, where air flows over a Nichrome wire, the heat from the wire is transferred to the air via convection. The rate at which heat is dissipated can be calculated using a convection coefficient, represented by the symbol 'h'. This coefficient depends on factors such as fluid velocity, its properties, the surface geometry, and the temperature difference between the surface and the fluid.

For a cylindrical wire, the convective surface area is given by the formula Ac = πDL, where D is the diameter and L is the length of the wire. The thermal energy transfer rate due to convection, Pc, is then determined as Pc = hAc(Tmax - T∞), signifying that higher convection coefficients and larger temperature differences will lead to greater heat transfer rates.
Radiation Heat Transfer
Radiation heat transfer refers to the emission of electromagnetic waves that carry energy away from the emitting surface. Unlike convection, radiation does not require a medium to transfer heat and can occur in a vacuum. In our exercise, the Nichrome wire also loses heat through radiation, which depends on the surface's emissivity (ε) and the temperature of both the surface and its surroundings.

The rate of heat loss due to radiation, Pr, can be expressed using the Stefan-Boltzmann law, described by the equation Pr = εσAc(Tmax4 - Tsur4), where σ is the Stefan-Boltzmann constant and Ac is the convective surface area, the same as for convection heat transfer. Materials with a higher emissivity will radiate more heat, and the temperature difference to the fourth power greatly influences the radiation heat loss.
Electrical Power Generation
The generation of electrical power in the context of the Nichrome wire heater is a conversion of electrical energy into thermal energy. This is described by Joule heating, where an electric current passing through a resistor (in this case, the Nichrome wire) converts the electrical energy into heat. The formula Pe = I2R succinctly demonstrates this relationship, where I is the electric current and R is the resistance of the wire.

This principle is widely utilized in electrical power appliances, where the control of current and resistance allows for the precise generation of desired amounts of heat. In industrial applications, such as electrical power generation plants, electromechanical conversions (like in turbines and generators) are used instead to convert mechanical energy into electrical power.
Thermal Conductivity
Thermal conductivity is an intrinsic physical property of a material that quantifies its ability to conduct heat. Within the given exercise, the thermal conductivity (k) of Nichrome governs how efficiently thermal energy is distributed through the wire. Materials with high thermal conductivity, such as metals, transfer heat quickly, whereas insulators, with low thermal conductivity, do so much slower.

In our scenario, the assumption is made that the temperature variations within the Nichrome wire are negligible, implying that heat conduction along the wire is efficient enough that it maintains a uniform temperature. However, for materials with low thermal conductivity, temperature gradients can occur, leading to differential heating along the source which can greatly affect the efficiency and performance of the heating element.

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Most popular questions from this chapter

A particular thermal system involves three objects of fixed shape with conduction resistances of \(R_{1}=1 \mathrm{~K} / \mathrm{W}\), \(R_{2}=2 \mathrm{~K} / \mathrm{W}\) and \(R_{3}=4 \mathrm{~K} / \mathrm{W}\), respectively. An objective is to minimize the total thermal resistance \(R_{\text {tot }}\) associated with a combination of \(R_{1}, R_{2}\), and \(R_{3}\). The chief engineer is willing to invest limited funds to specify an alternative material for just one of the three objects; the alternative material will have a thermal conductivity that is twice its nominal value. Which object (1, 2, or 3 ) should be fabricated of the higher thermal conductivity material to most significantly decrease \(R_{\text {tot }}\) ? Hint: Consider two cases, one for which the three thermal resistances are arranged in series, and the second for which the three resistances are arranged in parallel.

As seen in Problem \(3.109\), silicon carbide nanowires of diameter \(D=15 \mathrm{~nm}\) can be grown onto a solid silicon carbide surface by carefully depositing droplets of catalyst liquid onto a flat silicon carbide substrate. Silicon carbide nanowires grow upward from the deposited drops, and if the drops are deposited in a pattern, an array of nanowire fins can be grown, forming a silicon carbide nano-heat sink. Consider finned and unfinned electronics packages in which an extremely small, \(10 \mu \mathrm{m} \times 10 \mu \mathrm{m}\) electronics device is sandwiched between two \(d=100\)-nm-thick silicon carbide sheets. In both cases, the coolant is a dielectric liquid at \(20^{\circ} \mathrm{C}\). A heat transfer coefficient of \(h=1 \times 10^{5} \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) exists on the top and bottom of the unfinned package and on all surfaces of the exposed silicon carbide fins, which are each \(L=300 \mathrm{~nm}\) long. Each nano-heat sink includes a \(200 \times 200\) array of nanofins. Determine the maximum allowable heat rate that can be generated by the electronic device so that its temperature is maintained at \(T_{t}<85^{\circ} \mathrm{C}\) for the unfinned and finned packages.

During the initial stages of the growth of the nanowire of Problem 3.109, a slight perturbation of the liquid catalyst droplet can cause it to be suspended on the top of the nanowire in an off-center position. The resulting nonuniform deposition of solid at the solid-liquid interface can be manipulated to form engineered shapes such as a nanospring, that is characterized by a spring radius \(r\), spring pitch \(s\), overall chord length \(L_{c}\) (length running along the spring), and end-to-end length \(L\), as shown in the sketch. Consider a silicon carbide nanospring of diameter \(D=15 \mathrm{~nm}, r=30 \mathrm{~nm}, s=\) \(25 \mathrm{~nm}\), and \(L_{c}=425 \mathrm{~nm}\). From experiments, it is known that the average spring pitch \(\bar{s}\) varies with average temperature \(\bar{T}\) by the relation \(d \bar{s} / d \bar{T}=0.1 \mathrm{~nm} / \mathrm{K}\). Using this information, a student suggests that a nanoactuator can be constructed by connecting one end of the nanospring to a small heater and raising the temperature of that end of the nano spring above its initial value. Calculate the actuation distance \(\Delta L\) for conditions where \(h=10^{6} \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}, T_{\infty}=T_{i}=25^{\circ} \mathrm{C}\), with a base temperature of \(T_{b}=50^{\circ} \mathrm{C}\). If the base temperature can be controlled to within \(1^{\circ} \mathrm{C}\), calculate the accuracy to which the actuation distance can be controlled. Hint: Assume the spring radius does not change when the spring is heated. The overall spring length may be approximated by the formula,

Consider the conditions of Problem \(3.149\) but now allow for a tube wall thickness of \(5 \mathrm{~mm}\) (inner and outer diameters of 50 and \(60 \mathrm{~mm}\) ), a fin-to-tube thermal contact resistance of \(10^{-4} \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\), and the fact that the water temperature, \(T_{w}=350 \mathrm{~K}\), is known, not the tube surface temperature. The water-side convection coefficient is \(h_{w}=2000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the rate of heat transfer per unit tube length \((\mathrm{W} / \mathrm{m})\) to the water. What would be the separate effect of each of the following design changes on the heat rate: (i) elimination of the contact resistance; (ii) increasing the number of fins from four to eight; and (iii) changing the tube wall and fin material from copper to AISI 304 stainless steel \((k=20\) \(\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\) ?

An experimental arrangement for measuring the thermal conductivity of solid materials involves the use of two long rods that are equivalent in every respect, except that one is fabricated from a standard material of known thermal conductivity \(k_{\mathrm{A}}\) while the other is fabricated from the material whose thermal conductivity \(k_{\mathrm{B}}\) is desired. Both rods are attached at one end to a heat source of fixed temperature \(T_{b}\), are exposed to a fluid of temperature \(T_{\infty}\), and are instrumented with thermocouples to measure the temperature at a fixed distance \(x_{1}\) from the heat source. If the standard material is aluminum, with \(k_{\mathrm{A}}=200 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and measurements reveal values of \(T_{\mathrm{A}}=75^{\circ} \mathrm{C}\) and \(T_{\mathrm{B}}=60^{\circ} \mathrm{C}\) at \(x_{1}\) for \(T_{b}=100^{\circ} \mathrm{C}\) and \(T_{\infty}=25^{\circ} \mathrm{C}\), what is the thermal conductivity \(k_{\mathrm{B}}\) of the test material?

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