/*! 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 95 A procedure for measuring the th... [FREE SOLUTION] | 91Ó°ÊÓ

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A procedure for measuring the thermal conductivity of solids at elevated temperatures involves placement of a sample at the bottom of a large furnace. The sample is of thickness \(L\) and is placed in a square container of width \(W\) on a side. The sides are well insulated. The walls of the cavity are maintained at \(T_{w}\), while the bottom surface of the sample is maintained at a much lower temperature \(T_{e}\) by circulating coolant through the sample container. The sample surface is diffuse and gray with an emissivity \(\varepsilon_{s}\). Its temperature \(T_{s}\) is measured optically. (a) Neglecting convection effects, obtain an expression from which the sample thermal conductivity may be evaluated in terms of measured and known quantities \(\left(T_{w}, T_{s}, T_{c}, \varepsilon_{s}, L\right)\). The measurements are made under steady-state conditions. If \(T_{w}=1400 \mathrm{~K}, T_{s}=1000 \mathrm{~K}, \varepsilon_{s}=0.85, L=\) \(0.015 \mathrm{~m}\), and \(T_{c}=300 \mathrm{~K}\), what is the sample thermal conductivity? (b) If \(W=0.10 \mathrm{~m}\) and the coolant is water with a flow rate of \(\dot{m}_{c}=0.1 \mathrm{~kg} / \mathrm{s}\), is it reasonable to assume a uniform bottom surface temperature \(T_{c}\) ?

Short Answer

Expert verified
The sample thermal conductivity can be evaluated using the expression \(k = \frac{\varepsilon_{s} \sigma L (T_{w}^4 - T_{s}^4)}{T_{s} - T_{c}}\). Substituting the given values, we get \(k \approx 13.62 \, W / (m \cdot K)\). The assumption of a uniform bottom surface temperature \(T_{c}\) is reasonable due to the high thermal conductivity and specific heat capacity of water, as well as the large width and fast coolant flow rate.

Step by step solution

01

Define Fourier's Law for heat conduction

Fourier's Law states that the heat flux, \(q''\), is proportional to the temperature gradient, \(\frac{dT}{dx}\), and is given by: \(q'' = -k \frac{dT}{dx}\) Here, \(k\) is the thermal conductivity of the sample that we need to evaluate.
02

Set up a steady-state energy balance

Since we neglect convection, the net heat flux that enters the sample through the walls (\(q''_\text{rad}\)) must be equal to the net heat flux that leaves through the bottom surface by conduction (\(q''_\text{cond}\)), as the sample's temperature is maintained at a much lower value on the bottom surface. Therefore, we have: \(q''_\text{rad} = q''_\text{cond}\)
03

Express radiant heat flux

The radiant heat flux can be obtained using the Stefan-Boltzmann Law, considering the emissivity of the sample: \(q''_\text{rad} = \varepsilon_{s} \sigma (T_{w}^4 - T_{s}^4)\) Here, \(\varepsilon_{s}\) is the emissivity, \(\sigma\) is the Stefan-Boltzmann constant, and \(T_{w}\) and \(T_{s}\) are the temperatures of the cavity walls and sample surface, respectively.
04

Express conductive heat flux

We can express the conductive heat flux using Fourier's Law. We know that: \(q''_\text{cond} = k \frac{T_{s} - T_{c}}{L}\) Where \(k\) is the thermal conductivity, \(T_{c}\) is the temperature at the bottom surface, and \(L\) is the thickness of the sample.
05

Solve the energy balance equation

Now, we will equate the radiant and conductive heat flux expressions: \(\varepsilon_{s} \sigma (T_{w}^4 - T_{s}^4) = k \frac{T_{s} - T_{c}}{L}\) Then, we can solve for the thermal conductivity \(k\): \(k = \frac{\varepsilon_{s} \sigma L (T_{w}^4 - T_{s}^4)}{T_{s} - T_{c}}\)
06

Calculate the sample thermal conductivity

Now plug in the given values for \(T_{w} = 1400 \, K\), \(T_{s} = 1000 \, K\), \(\varepsilon_{s} = 0.85\), \(L = 0.015 \, m\), and \(T_{c} = 300 \, K\): \(k = \frac{0.85 \cdot 5.67 \times 10^{-8} \cdot 0.015 (1400^4 - 1000^4)}{1000 - 300}\) On solving, we get: \(k \approx 13.62 \, W / (m \cdot K)\)
07

Assess the reasonability of the assumption

The width of the container, \(W = 0.10 \, m\), and coolant flow rate \(\dot{m}_{c} = 0.1 \, kg / s\). Since water has high thermal conductivity and high specific heat capacity, and due to the large width compared to the thickness, the assumption that there is a uniform bottom surface temperature of \(T_{c}\) is reasonable. The flow rate of the coolant is fast enough to maintain a constant surface temperature, consequently minimizing temperature fluctuations along the bottom surface.

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Key Concepts

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

Fourier's Law
Fourier's Law is a foundational concept in thermal physics, connecting temperature gradients with thermal conduction. This law tells us how heat transfer occurs through materials due to a difference in temperature. The formula for Fourier's Law is written as:\[ q'' = -k \frac{dT}{dx} \]where:
  • \( q'' \) is the heat flux, representing the rate of heat transfer per unit area.
  • \( k \) is the thermal conductivity of the material, which describes how well the material can conduct heat.
  • \( \frac{dT}{dx} \) is the temperature gradient, showing how temperature changes with distance within the material.
Fourier's Law is widely applied when designing thermal systems, ensuring that materials can handle the expected thermal loads. In our context, it helps in determining the thermal conductivity of a sample by connecting it to known temperatures at the sample's interfaces.
Stefan-Boltzmann Law
The Stefan-Boltzmann Law is crucial for understanding how objects radiate heat. This law describes the radiant heat flux emitted by a surface, indicating how much energy is radiated as electromagnetic waves due to an object's temperature. The law is expressed as follows:\[ q''_\text{rad} = \varepsilon \sigma (T^4_\text{object} - T^4_\text{surrounding}) \]where:
  • \( q''_\text{rad} \) is the radiant heat flux, the power radiated per unit area.
  • \( \varepsilon \) is the emissivity of the surface, showing how effectively it radiates energy compared to a perfect black body.
  • \( \sigma \) is the Stefan-Boltzmann constant, approximately \( 5.67 \times 10^{-8} \, W/m^2K^4 \).
  • \( T_\text{object} \) and \( T_\text{surrounding} \) are the temperatures of the radiating object and its surroundings, respectively.
This law is especially important in the exercise context as it helps calculate the radiant heat exchange between the sample's surface and its surroundings, contributing to the total heat flux across the sample.
Radiant Heat Flux
Radiant heat flux refers to the energy transferred as heat through radiation, often influenced greatly by the temperature and properties of the surfaces involved. Unlike conduction, which requires direct contact, radiation can transfer heat across empty space. In the exercise, the radiant heat flux is a critical factor in determining the sample's thermal conductivity. This flux is defined by the Stefan-Boltzmann Law and depends upon:
  • Emissivity of the surface, \( \varepsilon_s \).
  • Surface temperature difference, emphasized by the objects' temperatures to the fourth power.
The effectiveness of heat transfer via radiation is highly dependent on surface characteristics like emissivity and temperature. High emissivity means better ability to emit energy as radiation, thus higher radiant heat flux.
Steady-State Energy Balance
In thermal analyses, a steady-state energy balance implies that all incoming and outgoing energy flows are equal, leading to no net energy change over time. This assumption allows simplification in calculations and is crucial in measuring thermal conductivity as seen in the exercise. Under steady-state conditions, the system reaches thermal equilibrium, meaning:
  • Heat entering a system equals the heat exiting the system.
  • Temperature distributions stabilize and do not change with time.
This concept is used to equate the radiant heat flux entering the sample with the conductive heat flux leaving it, ensuring an accurate calculation of thermal conductivity. By focusing on the steady-state energy balance, the calculation relies on maintained temperature differences across the sample at equilibrium, simplifying the computational process and ensuring consistent measurements.

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Most popular questions from this chapter

It is not uncommon for the night sky temperature in desert regions to drop to \(-40^{\circ} \mathrm{C}\). If the ambient air temperature is \(20^{\circ} \mathrm{C}\) and the convection coefticient for still air conditions is approximately \(5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), can a shallow pan of water freeze?

Estimate the wavelength corresponding to maximum emission from each of the following surfaces: the sun, a tungsten filament at \(2500 \mathrm{~K}\), a heated metal at \(1500 \mathrm{~K}\), human skin at \(305 \mathrm{~K}\), and a cryogenically cooled metal surface at \(60 \mathrm{~K}\). Estimate the fraction of the solar emission that is in the following spectral regions: the ultraviolet, the visible, and the infrared.

A furnace with an aperture of 20 -mm diameter and emissive power of \(3.72 \times 10^{5} \mathrm{~W} / \mathrm{m}^{2}\) is used to calibrate a heat flux gage having a sensitive area of \(1.6 \times 10^{-5} \mathrm{~m}^{2}\). (a) At what distance, measured along a normal from the aperture, should the gage be positioned to receive irradiation of \(1000 \mathrm{~W} / \mathrm{m}^{2}\) ? (b) If the gage is tilted off normal by \(20^{\circ}\), what will be its irradiation? (c) For tilt angles of 0,20 , and \(60^{\circ}\), plot the gage irradiation as a function of the separation distance for values ranging from 100 to \(300 \mathrm{~mm}\).

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 outside 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. 12.108 Neglecting the effects of radiation absorption, emission, and scattering within their atmospheres, calculate the average temperature of Earth, Venus, and Mars assuming diffuse, gray behavior. The average distance from the sun of each of the three planets, \(L_{s p}\), along with their measured average temperatures, \(\bar{T}_{p}\), are shown in the table below. Based upon a comparison of the calculated and measured average temperatures, which planet is most affected by radiation transfer in its atmosphere? \begin{tabular}{lcc} \hline Planet & \(L_{x-p}(\mathbf{m})\) & \(\bar{T}_{p}(\mathbf{K})\) \\ \hline Venus & \(1.08 \times 10^{11}\) & 735 \\ Earth & \(1.50 \times 10^{11}\) & 287 \\ Mars & \(2.30 \times 10^{11}\) & 227 \\ \hline \end{tabular}

A proposed method for generating electricity from solar irradiation is to concentrate the irradiation into a cavity that is placed within a large container of a salt with a high melting temperature. If all heat losses are neglected, part of the solar irradiation entering the cavity is used to melt the salt while the remainder is used to power a Rankine cycle. (The salt is melted during the day and is resolidified at night in order to generate electricity around the clock.) Consider conditions for which the solar power entering the cavity is \(q_{\mathrm{sal}}=7.50 \mathrm{MW}\) and the time rate of change of energy stored in the salt is \(\dot{E}_{\mathrm{st}}=3.45 \mathrm{MW}\). For a cavity opening of diameter \(D_{s}=1 \mathrm{~m}\), determine the heat transfer to the Rankine cycle, \(q_{R}\). The temperature of the salt is maintained at its melting point, \(T_{\text {salt }}=T_{\text {m }}=1000^{\circ} \mathrm{C}\). Neglect heat loss by convection and irradiation from the surroundings.

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