/*! 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 114 The temperature of a flowing gas... [FREE SOLUTION] | 91Ó°ÊÓ

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The temperature of a flowing gas is to be measured with a thermocouple junction and wire stretched between two legs of a sting, a wind tunnel test fixture. The junction is formed by butt-welding two wires of different material, as shown in the schematic. For wires of diameter \(D=125 \mu \mathrm{m}\) and a convection coefficient of \(h=700 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the minimum separation distance between the two legs of the sting, \(L=L_{1}+L_{2}\), to ensure that the sting temperature does not influence the junction temperature and, in turn, invalidate the gas temperature measurement. Consider two different types of thermocouple junctions consisting of (i) copper and constantan wires and (ii) chromel and alumel wires. Evaluate the thermal conductivity of copper and constantan at \(T=300 \mathrm{~K}\). Use \(k_{\mathrm{Ch}}=19 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and \(k_{\mathrm{Al}}=29 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) for the thermal conductivities of the chromel and alumel wires, respectively.

Short Answer

Expert verified
For a copper-constantan junction, the minimum separation distance between the two legs of the sting can be calculated using: \[ L = D\left(\frac{(T_\mathrm{j} - T_\mathrm{g})}{Q_\mathrm{cond}}\right)\left(\frac{1}{k_\mathrm{Cu}} + \frac{1}{k_\mathrm{Co}}\right) \] And for a chromel-alumel junction, the minimum separation distance can be calculated using: \[ L = D\left(\frac{(T_\mathrm{j} - T_\mathrm{g})}{Q_\mathrm{cond}}\right)\left(\frac{1}{k_\mathrm{Ch}} + \frac{1}{k_\mathrm{Al}}\right) \] Plug in the given values for diameter, convection coefficient, and thermal conductivity, and calculate the minimum separation distances for both types of thermocouples.

Step by step solution

01

Compute the thermal conductivities for copper and constantan at \(T = 300\,\mathrm{K}\)

First, we need to find the thermal conductivities of copper and constantan at \(300\,\mathrm{K}\). According to the literature, their thermal conductivities at this temperature can be approximated as: \(k_\text{Cu}\) = 398 W/m·K \(k_\mathrm{Co}\) = 22 W/m·K Now, we have the thermal conductivities for all the materials: copper, constantan, chromel, and alumel.
02

Compute the thermal resistance of each wire

Next, we need to calculate the thermal resistance of the wires, which can be found using the formula: \[ R_\mathrm{cond} = \frac{L_i}{k_\mathrm{i}A_\mathrm{i}} \] where \(R_\mathrm{cond}\) is the conduction thermal resistance, \(L_{i}\) is the length of the wire of material \(i\), \(k_\mathrm{i}\) is the thermal conductivity of material \(i\), and \(A_\mathrm{i}\) is the cross-sectional area of the wire of material \(i\). For a cylindrical wire, the cross-sectional area can be expressed as: \[A_\mathrm{i} = \frac{\pi D^2}{4}\] Now, we can define the total thermal resistance of the wire as: \[ R_\mathrm{total} = R_\mathrm{Cu} + R_\mathrm{Co} = \frac{L_1}{k_\mathrm{Cu}A_\mathrm{Cu}} + \frac{L_2}{k_\mathrm{Co}A_\mathrm{Co}} \] For chromel-alumel, the thermal resistance will be: \[ R_\mathrm{total} = R_\mathrm{Ch} + R_\mathrm{Al} = \frac{L_1}{k_\mathrm{Ch}A_\mathrm{Ch}} + \frac{L_2}{k_\mathrm{Al}A_\mathrm{Al}} \]
03

Compute the total heat transfer from the wires to the gas

Now, let's compute the total heat transfer from the wires to the gas, which involves convection. The heat transfer due to convection can be expressed as: \[ Q_\mathrm{conv} = hA_\mathrm{s}(T_\mathrm{j} - T_\mathrm{g}) \] where \(Q_\mathrm{conv}\) is the convective heat transfer, \(T_j\) is the junction temperature, \(T_\mathrm{g}\) is the gas temperature, and \(A_\mathrm{s}\) is the surface area of the wire in contact with the gas. Since the thermocouple junction does not influence the gas temperature measurement, the heat transfer from both wires should be equal. Therefore, the convective heat transfer from the copper or chromel wire to the gas equals the convective heat transfer from the constantan or alumel wire to the gas. \[ Q_\mathrm{conv} = Q_\mathrm{Cu} = Q_\mathrm{Co} \quad\text{or}\quad Q_\mathrm{conv} = Q_\mathrm{Ch} = Q_\mathrm{Al} \]
04

Determine the minimum separation distance between the two legs of the sting

The junction temperature, \(T_\mathrm{j}\), remains constant, and the heat transfer through conduction should equal the heat transfer through convection: \[ Q_\mathrm{cond} = Q_\mathrm{conv} \] Hence, we can equate the thermal resistance times the heat transfer to the convective heat transfer: \[ R_\mathrm{total}Q_\mathrm{cond} = hA_\mathrm{s}(T_\mathrm{j} - T_\mathrm{g}) \] Using the relationships from Steps 2 and 3, we can relate the lengths \(L_1\) and \(L_2\) to the gas temperature and the junction temperature: \[ \frac{L_1}{k_\mathrm{Cu}A_\mathrm{Cu}} + \frac{L_2}{k_\mathrm{Co}A_\mathrm{Co}} = \frac{hA_\mathrm{s}(T_\mathrm{j} - T_\mathrm{g})}{Q_\mathrm{cond}} \] Now, we can solve for the minimum separation distance: \[ L = L_1 + L_2 = D\left(\frac{(T_\mathrm{j} - T_\mathrm{g})}{Q_\mathrm{cond}}\right)\left(\frac{1}{k_\mathrm{Cu}} + \frac{1}{k_\mathrm{Co}}\right) \] Similarly, for the chromel-alumel junction: \[ L = L_1 + L_2 = D\left(\frac{(T_\mathrm{j} - T_\mathrm{g})}{Q_\mathrm{cond}}\right)\left(\frac{1}{k_\mathrm{Ch}} + \frac{1}{k_\mathrm{Al}}\right) \] Finally, plug in the given values for diameter, convection coefficient, and thermal conductivity, and calculate the minimum separation distances for both types of thermocouples.

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Key Concepts

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

Thermocouple
A thermocouple is a simple yet powerful device used to measure temperatures. It relies on the principle that when two different types of metals are joined together at one end and exposed to varying temperatures, they generate a voltage. This voltage is directly related to the temperature difference between the two ends of the wires.
In the scenario of our exercise, specially chosen metals are joined to form the thermocouple junction. For this exercise, the junction combines copper and constantan, or chromel and alumel. The thermocouple measures the temperature of the flowing gas in the wind tunnel test fixture, where the junction is critical in providing accurate readings.
The choice of wire materials affects the thermocouple's sensitivity and operational range. Copper and constantan provide different responses compared to chromel and alumel due to their distinct physical properties and thermal conductivities.
Thermal Conductivity
Thermal conductivity is a physical property of materials that describes their ability to conduct heat. It is an essential parameter in assessing how well heat can flow through the materials used in the thermocouple device.
In our exercise, we compute the thermal conductivities of copper, constantan, chromel, and alumel, which are necessary to assess the heat transfer efficiency. At a given temperature of 300K, copper has a thermal conductivity of 398 W/m·K, indicating it is excellent at conducting heat. In contrast, constantan has a thermal conductivity of 22 W/m·K, showing it is much less efficient at heat conduction compared to copper.
The chromel and alumel wires used in another type of thermocouple have conductivities of 19 W/m·K and 29 W/m·K, respectively. These values influence the rate at which heat can travel through the wires and ultimately affect the accuracy of the temperature measurement provided by the thermocouple.
Convection
Convection is one of the modes of heat transfer and occurs when heat is transferred by the movement of fluids such as gases or liquids. In this exercise, convection plays a key role in transferring heat from the wires of the thermocouple to the surrounding gas.
The convection coefficient, denoted as \(h\), is used to measure the efficiency of this process. For the wind tunnel scenario given, the convection coefficient is \(h = 700 \text{ W/m}^2 \cdot \text{K}\). This high value indicates efficient heat transfer from the thermocouple wires to the gas.
The convective heat transfer equation is \(Q_{\text{conv}} = hA_s(T_j - T_g)\), where \(A_s\) is the surface area of the wire in contact with the gas, \(T_j\) is the junction temperature, and \(T_g\) is the gas temperature. By balancing the convective heat transfer with the heat conducted along the wires, we ensure the thermocouple provides accurate information about the gas temperature.
Heat Resistance
Heat resistance, specifically thermal resistance, is the opposition to heat flow through a material or an assembly of materials. In this exercise, it determines how much the wire materials resist the flow of heat, affecting the temperature measured by the thermocouple.
We calculate thermal resistance using the formula \(R_{\text{cond}} = \frac{L_i}{k_iA_i}\), where \(L_i\) is the length of the wire, \(k_i\) is its thermal conductivity, and \(A_i\) is the cross-sectional area. Each wire's thermal resistance contributes to the total resistance, influencing how well each wire conducts heat away from the junction.
Accurate evaluation of heat resistance is crucial for determining the minimum separation distance \(L = L_1 + L_2\) between the sting's legs. This ensures that the sting temperature does not affect the thermocouple junction's temperature, allowing precise measurements of the gas temperature. We demonstrate that understanding the heat resistance properties aids in assessing the efficiency of heat flow in the thermocouple circuit.

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Most popular questions from this chapter

The evaporator section of a refrigeration unit consists of thin-walled, 10-mm- diameter tubes through which refrigerant passes at a temperature of \(-18^{\circ} \mathrm{C}\). Air is cooled as it flows over the tubes, maintaining a surface convection coefficient of \(100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and is subsequently routed to the refrigerator compartment. (a) For the foregoing conditions and an air temperature of \(-3^{\circ} \mathrm{C}\), what is the rate at which heat is extracted from the air per unit tube length? (b) If the refrigerator's defrost unit malfunctions, frost will slowly accumulate on the outer tube surface. Assess the effect of frost formation on the cooling capacity of a tube for frost layer thicknesses in the range \(0 \leq \delta \leq 4 \mathrm{~mm}\). Frost may be assumed to have a thermal conductivity of \(0.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). (c) The refrigerator is disconnected after the defrost unit malfunctions and a 2-mm-thick layer of frost has formed. If the tubes are in ambient air for which \(T_{\infty}=20^{\circ} \mathrm{C}\) and natural convection maintains a convection coefficient of \(2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), how long will it take for the frost to melt? The frost may be assumed to have a mass density of \(700 \mathrm{~kg} / \mathrm{m}^{3}\) and a latent heat of fusion of \(334 \mathrm{~kJ} / \mathrm{kg}\).

Consider a tube wall of inner and outer radii \(r_{i}\) and \(r_{o}\), whose temperatures are maintained at \(T_{i}\) and \(T_{o}\), respectively. The thermal conductivity of the cylinder is temperature dependent and may be represented by an expression of the form \(k=k_{o}(1+a T)\), where \(k_{o}\) and \(a\) are constants. Obtain an expression for the heat transfer per unit length of the tube. What is the thermal resistance of the tube wall?

A composite wall separates combustion gases at \(2600^{\circ} \mathrm{C}\) from a liquid coolant at \(100^{\circ} \mathrm{C}\), with gas- and liquid-side convection coefficients of 50 and 1000 \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The wall is composed of a \(10-\mathrm{mm}\)-thick layer of beryllium oxide on the gas side and a 20 -mm-thick slab of stainless steel (AISI 304) on the liquid side. The contact resistance between the oxide and the steel is \(0.05 \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\). What is the heat loss per unit surface area of the composite? Sketch the temperature distribution from the gas to the liquid.

As a means of enhancing heat transfer from highperformance logic chips, it is common to attach a heat \(\sin k\) to the chip surface in order to increase the surface area available for convection heat transfer. Because of the ease with which it may be manufactured (by taking orthogonal sawcuts in a block of material), an attractive option is to use a heat sink consisting of an array of square fins of width \(w\) on a side. The spacing between adjoining fins would be determined by the width of the sawblade, with the sum of this spacing and the fin width designated as the fin pitch \(S\). The method by which the heat sink is joined to the chip would determine the interfacial contact resistance, \(R_{t, c^{*}}^{n}\) Consider a square chip of width \(W_{c}=16 \mathrm{~mm}\) and conditions for which cooling is provided by a dielectric liquid with \(T_{\infty}=25^{\circ} \mathrm{C}\) and \(h=1500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The heat \(\operatorname{sink}\) is fabricated from copper \((k=400 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\), and its characteristic dimensions are \(w=0.25 \mathrm{~mm}\), \(S=0.50 \mathrm{~mm}, L_{f}=6 \mathrm{~mm}\), and \(L_{b}=3 \mathrm{~mm}\). The prescribed values of \(w\) and \(S\) represent minima imposed by manufacturing constraints and the need to maintain adequate flow in the passages between fins. (a) If a metallurgical joint provides a contact resistance of \(R_{t, c}^{\prime \prime}=5 \times 10^{-6} \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\) and the maximum allowable chip temperature is \(85^{\circ} \mathrm{C}\), what is the maximum allowable chip power dissipation \(q_{c} ?\) Assume all of the heat to be transferred through the heat sink. (b) It may be possible to increase the heat dissipation by increasing \(w\), subject to the constraint that \((S-w) \geq 0.25 \mathrm{~mm}\), and/or increasing \(L_{f}\) (subject to manufacturing constraints that \(L_{f} \leq 10 \mathrm{~mm}\) ). Assess the effect of such changes.

A storage tank consists of a cylindrical section that has a length and inner diameter of \(L=2 \mathrm{~m}\) and \(D_{i}=1 \mathrm{~m}\), respectively, and two hemispherical end sections. The tank is constructed from 20-mm-thick glass (Pyrex) and is exposed to ambient air for which the temperature is \(300 \mathrm{~K}\) and the convection coefficient is \(10 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The tank is used to store heated oil, which maintains the inner surface at a temperature of \(400 \mathrm{~K}\). Determine the electrical power that must be supplied to a heater submerged in the oil if the prescribed conditions are to be maintained. Radiation effects may be neglected, and the Pyrex may be assumed to have a thermal conductivity of \(1.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

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