/*! 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 76 A temperature sensor imbedded in... [FREE SOLUTION] | 91Ó°ÊÓ

91Ó°ÊÓ

A temperature sensor imbedded in the tip of a small tube having a diffuse, gray surface with an emissivity of \(0.8\) is centrally positioned within a large air-conditioned toom whose walls and air temperature are 30 and \(20^{\circ} \mathrm{C}\), respectively. (a) What temperature will the sensor indicate if the convection coefficient between the sensot tube and the air is \(5 \mathrm{~W} / \mathrm{m}^{2}\) - K? (b) What would be the effect of using a fan to induce airflow over the tube? Plot the sensor temperature as a function of the convection cocfficient for \(2 \leq h \leq 25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and values of \(\mathrm{e}=0.2,0.5\). and \(0.8\).

Short Answer

Expert verified
(a) The sensor indicates approximately \(23.2^{\circ} \mathrm{C}\). (b) Increasing airflow decreases sensor temperature.

Step by step solution

01

Define Given Parameters

- Emissivity of the sensor surface, \(\varepsilon = 0.8\).- Convection coefficient, \(h = 5 \, \mathrm{W/m^2 \cdot K}\).- Air temperature, \(T_{\infty} = 20^{\circ} \mathrm{C}\).- Wall temperature, \(T_{surr} = 30^{\circ} \mathrm{C}\).
02

Understanding Heat Exchange

The sensor exchanges heat with both the surrounding air and the walls through convection and radiation, respectively. The equilibrium occurs when the heat gained and lost by the sensor is equal.
03

Setup the Energy Balance Equation

The energy balance equation for the sensor can be expressed as: \[ q_{conv} + q_{rad} = 0 \]where \( q_{conv} = h A (T_s - T_{\infty}) \) and \( q_{rad} = \varepsilon \sigma A (T_s^4 - T_{surr}^4) \). Here, \(T_s\) is the sensor temperature in Kelvin and \(\sigma = 5.67 \times 10^{-8} \, \mathrm{W/m^2 \cdot K^4}\) is the Stefan-Boltzmann constant.
04

Solve for Sensor Temperature \(T_s\)

Substituting the given values, the equation to find the sensor temperature \(T_s\) is:\[ h (T_s - 293) + \varepsilon \sigma (T_s^4 - 303^4) = 0 \]Since this is a nonlinear equation in \(T_s\), solving it analytically is complex and often requires numerical methods.
05

Temperature Value for Part (a)

Solving the above equation using suitable numerical methods (e.g., the Newton-Raphson method), we find that the temperature indicated by the sensor is approximately \(23.2^{\circ} \mathrm{C}\).
06

Influence of Enhanced Convection via a Fan

Increasing the convection coefficient \(h\) by using a fan affects the convection term \(q_{conv}\), leading to a decrease in \(T_s\) as higher \(h\) values enhance heat loss to the air.
07

Plotting Sensor Temperature vs Convection Coefficient

To analyze how changing the convection coefficient from 2 to 25 with emissivities \(e = 0.2, 0.5, 0.8\) affects sensor temperature, we calculate \(T_s\) for each condition, generating curves for each emissivity. The plot indicates \(T_s\) decreases nonlinearly with increase in \(h\). This is done programmatically using computational software.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with 91Ó°ÊÓ!

Key Concepts

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

Radiation
Radiation is a mode of heat transfer that involves the emission of energy in the form of electromagnetic waves. This energy can travel through a vacuum and doesn’t require a medium, making it a significant factor in heat exchange, especially in environments where physical contact is limited.
In the context of the sensor in an air-conditioned room, radiation is the heat exchange process between the sensor and the surrounding walls. The electromagnetic waves are emitted and absorbed based on the temperature difference and the emissivity of the surfaces involved.
The heat transferred as radiation can be quantified using the Stefan-Boltzmann law, which is represented by the equation:\[ q_{rad} = \varepsilon \sigma A (T_s^4 - T_{surr}^4) \]where \( \varepsilon \) is the emissivity of the surface, \( \sigma \) is the Stefan-Boltzmann constant, and \( A \) is the area. The temperatures involved are in Kelvin, highlighting the importance of considering absolute temperatures when dealing with radiative heat transfer.
Convection
Convection is the process of heat transfer through the movement of fluid (liquid or gas) particles. It involves the transfer of heat from one place to another by the physical movement of molecules within fluids.
The rate of heat transfer by convection is influenced by the convection coefficient, often denoted by \( h \), which depends on several factors including fluid properties, flow velocity, and surface geometries. This coefficient represents how effectively heat is transferred between the surface and the fluid.
In the exercise, convection heat transfer occurs between the air in the room and the sensor surface. The energy balance for convection can be given as:\[ q_{conv} = h A (T_s - T_\infty) \]where \( T_s \) is the temperature of the sensor, and \( T_\infty \) is the air temperature. By understanding this relationship, we can infer how changes in air movement, such as through the introduction of a fan, can impact the sensor's temperature reading.
Emissivity
Emissivity, denoted by \( \varepsilon \), is a measure of a material's ability to emit thermal radiation compared to an ideal blackbody. A value of \( 1 \) signifies a perfect emitter, while a value of \( 0 \) indicates no emission capability.
The emissivity of a material affects how it exchanges heat through radiation. In our scenario, the emissivity of the sensor's surface is \( 0.8 \), meaning it has a reasonably high capacity to emit thermal radiation compared to an ideal black body.
This parameter is crucial in calculating the radiative heat transfer, as seen in the Stefan-Boltzmann law expression where emissivity influences the amount of thermal radiation emitted. Understanding emissivity allows us to predict how efficiently an object will radiate heat away, impacting the energy balance of systems involving thermal interactions.
Energy Balance Equation
The energy balance equation is fundamental in determining the state of thermal equilibrium for systems like our temperature sensor. This equation ensures that the total energy flow into and out of a system reaches balance, establishing a constant system temperature over time.
For the exercise, the energy balance is expressed as the sum of the heat transferred by convection and radiation equaling zero:\[ q_{conv} + q_{rad} = 0 \]This equation underpins the principle that the thermal energy entering the sensor is equal to the energy leaving it.
The convection component accounts for heat exchanged with the air, while the radiation component considers heat exchange with the wall. By solving this equation, we can predict the sensor's temperature, illustrating how energy conservation principles govern practical heat transfer scenarios.

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Solar irradiation of \(1100 \mathrm{~W} / \mathrm{m}^{2}\) is incident on a large, flat, horizontal metal roof on a day when the wind blowing over the roof causes a convection heat transfer coefficient of \(25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The cutside air temperature is \(27^{\circ} \mathrm{C}\), the metal surface absorptivity for incident solar radiation is \(0.60\), the metal surface emissivity is \(0.20\), and the roof is well insulated from below. (a) Estimate the roof temperature under steady-state conditions. (b) Explore the effect of changes in the absorptivity. emissivity, and convection coefficient on the steady-state temperature.

A shallow layer of water is exposed to the natural environment as shown.Consider conditions for which the solar and atmospheric irmadiations are \(G_{S}=600 \mathrm{~W} / \mathrm{m}^{2}\) and \(G_{A}=\) \(300 \mathrm{~W} / \mathrm{m}^{2}\), respectively, and the air temperature and relative humidity are \(T_{w}=27^{\circ} \mathrm{C}\) and \(\phi_{w}=0.50\). respectively, The reflectivities of the water surface to the solar and atmospheric irradiation are \(\rho_{5}=0.3\) and \(\rho_{A}=0\), respectively, while the surface emissivity is \(\varepsilon=0.97\). The convection heat transfer coefficient at the air-water interface is \(h=25 \mathrm{~W} / \mathrm{m}^{2}-\mathrm{K}\). If the water is at \(27^{\circ} \mathrm{C}\), will this temperature increase or decrease with time?

A horizontal, opaque surface at a steady-sate temperature of \(77^{\circ} \mathrm{C}\) is exposed in an airflow having a free stream temperature of \(27^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of \(28 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The emissive power of the surface is \(628 \mathrm{~W} / \mathrm{m}^{2}\), the irradiation is \(1380 \mathrm{~W} / \mathrm{m}^{2}\), and the reflectivity is \(0.40\). Determine the absorptivity of the surface. Determine the act ractiation heat transfer rate for this surface. Is this heat transfer to the wurface or from the surface? Determine the combined heat transfer rate for the surface. Is this heat transfer to the surface or from the surface?

A roof-cooling system, which operates by maintaining a thin film of water on the roof surface, may be used to reduce air-conditioning costs or to maintain a cooler environment in nonconditioned buildings. To determine the effectiveness of such a system, consider a sheet metal roof for which the solar absorptivity \(\alpha_{s}\) is \(0.50\) and the hemispherical emissivity \(\varepsilon\) is \(0.3\). Representative conditions correspond to a surface convection coefficient \(h\) of \(20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), a solar irradiation \(G_{S}\) of \(700 \mathrm{~W} / \mathrm{m}^{2}\), a sky temperature of \(-10^{\circ} \mathrm{C}\), an utmospheric temperature of \(30^{\circ} \mathrm{C}\), and a relutive humidity of \(65 \%\). The roof may be assumed to be well insulated from below. Determine the roof surface temperature without the water film. Assuming the film and roof surface temperatures to be cqual, determine the surface temperature with the film. The solar absorptivity and the hemispherical emissivity of the film-surface combination are \(\alpha_{s}=0.8\) and \(\varepsilon=0.9\), respectively.

One scheme for extending the operation of gas turbine blades to higher temperatures involves applying a ceramic coating to the surfaces of blades fabricated from a superalloy such as inconel. To assess the reliability of such coatings, an apparatus has been developed for testing samples under laboratory conditions. The sample is placed at the bottom of a large vacuum chamber whose walls are cryogenically cooled and which is equipped with a radiation detector at the top surface. The detector has a surface area of \(A_{d}=\) \(10^{-5} \mathrm{~m}^{2}\), is located at a distance of \(L_{2-d}=1 \mathrm{~m}\) from the sample, and views radiation originating from a portion of the ceramic surface having an area of \(\Delta A_{c}=10^{-4}\) \(m^{2}\). An electric heater attached to the bottom of the sample dissipates a uniform heat flux, \(q_{h}^{n}\), which is transferred upward through the sample. The botiom of the heater and sides of the sample are well insulated. Consider conditions for which a ceramic coating of thickness \(L_{\gamma}=0.5 \mathrm{~mm}\) and thermal conductivity \(k_{\mathrm{c}}=6 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) has been sprayed on a metal substrute of thickness \(L,=8 \mathrm{~mm}\) and thermal conductivity \(k_{3}=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The opaque surface of the ceramic may be approximated as diffuse and gray. with a total, hemispherical emissivity of \(\varepsilon_{c}=0.8\). (a) Consider steady-state conditions for which the bottom surface of the substrate is maintained at \(T_{1}=1500 \mathrm{~K}\), while the chamber walls (including the surface of the radistion detector) are maintained at \(T_{\mathrm{w}}=90 \mathrm{~K}\). Assuming negligible thermal contact resistance at the ceramic-substrate interface, determine the ceramic top surface temperature \(T_{2}\) and the hest flux \(q_{\hbar-}^{\prime \prime}\) (b) For the prescribed conditions, what is the rate at which radiation emitted by the ceramic is intercepted by the detector? (c) After repeated experiments, numerous cracks develop at the ceramic- substrate interface, creating an interfacial thermal contact resistance. If \(T_{w}\) and \(q_{h}^{\prime \prime}\) are maintained at the conditions associated with part (a), will \(T_{1}\) increase, decrease, or remain the same? Similarly, will \(T_{2}\) increase, decrease, or remain the same? In cach case, justify your answer.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.