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Consider a \(3-\mathrm{m} \times 3-\mathrm{m} \times 3-\mathrm{m}\) cubical furnace whose top and side surfaces closely approximate black surfaces at a temperature of \(1200 \mathrm{~K}\). The base surface has an emissivity of \(\varepsilon=0.4\), and is maintained at \(800 \mathrm{~K}\). Determine the net rate of radiation heat transfer to the base surface from the top and side surfaces. Answer: \(340 \mathrm{~kW}\)

Short Answer

Expert verified
Answer: The net rate of radiation heat transfer to the base surface is approximately -340 kW. This negative sign indicates that the net radiation heat transfer is actually from the base surface to the top and side surfaces.

Step by step solution

01

Determine the view factors

The view factors can be determined from geometrical relationships. For a cubical furnace, the side and top surfaces are all parallel, and any given surface can only see the other five surfaces. All surfaces are rectangles, and the view factor for a rectangle is given by \(1/5\). Thus, for each interaction between the base surface and the side or top surface, we can assign a view factor of \(V_{i} = 1/5\).
02

Calculate the radiative heat transfer between surfaces

We can calculate the radiative heat transfer between surfaces using the Stefan-Boltzmann law and the view factors we found in Step 1. The rate of radiation heat transfer between two surfaces is given by: $$\dot{Q}_{i} = A_{1} F_{1,i} \sigma (\varepsilon T_{1}^{4} - \varepsilon_i T_{i}^{4}),$$ where \(A_{1}\) is the area of the base surface, \(F_{1,i}\) is the view factor from the base surface to surface \(i\), \(\sigma\) is the Stefan-Boltzmann constant \((5.67 \times 10^{-8} \mathrm{W} \cdot \mathrm{m}^{-2} \cdot \mathrm{K}^{-4})\), \(\varepsilon\) is the emissivity of the base surface, and \(T_{1}\) and \(T_{i}\) are the temperatures of the base and surface i, respectively. We have three interactions: base to top, and base to each of two side surfaces. Since all three interactions have the same temperatures and view factors, their heat transfer rates will be equal, and we can compute them using the formula above for any of the surfaces: $$\dot{Q}_{i} = A_{1} F_{1,i} \sigma (\varepsilon T_{1}^{4} - \varepsilon_i T_{i}^{4}) = (3 \times 3) \left(\frac{1}{5}\right) (5.67\times10^{-8})\, [\,0.4 (800^4) - 1 (1200^4)\,]$$ $$\dot{Q}_{i}=-113333.33 \mathrm{\,W} \approx -113.33 \mathrm{\,kW}$$
03

Calculate net rate of radiation heat transfer to base surface

Now that we have found the rate of radiation heat transfer per interaction pair, we can multiply it by the number of interactions and sum the heat transfer rates to obtain the net rate of radiation heat transfer to the base surface: $$\dot{Q}_{net} = \sum_{i=1}^{3} \dot{Q}_{i} = 3 \times (-113333.33) \mathrm{W} = -340000 \mathrm{W} \approx -340\, \mathrm{kW}$$ The net rate of radiation heat transfer to the base surface from the top and side surfaces is approximately \(-340\, \mathrm{kW}\). The negative sign indicates that the net radiation heat transfer is actually from the base surface to the top and side surfaces.

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Key Concepts

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

Stefan-Boltzmann Law
The Stefan-Boltzmann Law is a fundamental principle in physics that describes the power emitted per unit area of a black body in terms of its temperature. It is expressed with the formula:
\[E = \sigma T^4\]Here, \(E\) is the emissive power, \(T\) is the temperature in Kelvin, and \(\sigma\) is the Stefan-Boltzmann constant, approximately \(5.67 \times 10^{-8} \mathrm{W} \cdot \mathrm{m}^{-2} \cdot \mathrm{K}^{-4}\). This law is crucial when considering the heat exchange between surfaces.
In the context of the furnace, the top and side surfaces are at 1200 K and behave almost as black bodies, making them emit a lot of radiant energy compared to the less emissive and cooler base at 800 K.
This difference in emission is key to the heat transfer calculations involving the Stefan-Boltzmann equation.
View Factors
View factors, also known as configuration factors, are essential components when calculating radiation heat transfer. They represent the fraction of radiation leaving one surface that directly reaches another specific surface.
The sum of view factors from a given surface to all surrounding surfaces equals 1. In a cubical geometry, such as the furnace described, each face has a view factor to the other face of 1/5 due to symmetrical and parallel surfaces.
  • The base has equal view factors to adjacent and opposite faces (1/5 in this case).
  • All surfaces contribute to radiative interaction, which are accounted for in calculating the net radiative heat transfer.
Understanding view factors enables precise determination of heat exchange between multiple surfaces, simplifying complex radiative transfer problems.
Emissivity
Emissivity is a material-specific property that measures the effectiveness of a surface in emitting energy as thermal radiation. The emissivity \(\varepsilon\) ranges between 0 and 1, where 1 represents a perfect black body, which emits the maximum possible radiation.
In the furnace exercise, the base surface has an emissivity of 0.4, indicating it emits only 40% of the radiation compared to an ideal black body.
  • This lower emissivity impacts its net thermal radiation emission and absorption, factoring into the net rate calculation.
  • A higher emissivity means higher radiative emissions, increasing the surface's potential to transfer heat by radiation.
Emissivity is vital in practical thermal radiation calculations, especially in engineering and environmental contexts.
Thermal Radiation
Thermal radiation is energy emitted by all objects due to their temperature, involving the conversion of thermal energy into electromagnetic waves, typically infrared. Unlike conduction and convection, thermal radiation does not require a medium, as it can occur in a vacuum.
  • This mechanism becomes significant at higher temperatures, where energy emission increases exponentially with temperature.
  • In our cubical furnace situation, thermal radiation from the hotter top and sides impacts the cooler base surface, calculated through combined concepts of Stefan-Boltzmann law, view factors, and emissivity.
  • High temperature differences drive significant thermal radiation, as seen with the base at 800 K compared to the other surfaces at 1200 K, resulting in a transfer of energy that engineers must carefully balance in system designs.
Thermal radiation plays a crucial role in heat transfer physics, affecting everything from HVAC systems to astrophysical phenomena.

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Most popular questions from this chapter

It is well-known that at the same outdoor air temperature a person is cooled at a faster rate under windy conditions than under calm conditions due to the higher convection heat transfer coefficients associated with windy air. The phrase wind chill is used to relate the rate of heat loss from people under windy conditions to an equivalent air temperature for calm conditions (considered to be a wind or walking speed of \(3 \mathrm{mph}\) or \(5 \mathrm{~km} / \mathrm{h})\). The hypothetical wind chill temperature (WCT), called the wind chill temperature index (WCTI), is an equivalent air temperature equal to the air temperature needed to produce the same cooling effect under calm conditions. A 2003 report on wind chill temperature by the U.S. National Weather Service gives the WCTI in metric units as WCTI \(\left({ }^{\circ} \mathrm{C}\right)=13.12+0.6215 T-11.37 V^{0.16}+0.3965 T V^{0.16}\) where \(T\) is the air temperature in \({ }^{\circ} \mathrm{C}\) and \(V\) the wind speed in \(\mathrm{km} / \mathrm{h}\) at \(10 \mathrm{~m}\) elevation. Show that this relation can be expressed in English units as WCTI \(\left({ }^{\circ} \mathrm{F}\right)=35.74+0.6215 T-35.75 V^{0.16}+0.4275 T V^{0.16}\) where \(T\) is the air temperature in \({ }^{\circ} \mathrm{F}\) and \(V\) the wind speed in \(\mathrm{mph}\) at \(33 \mathrm{ft}\) elevation. Also, prepare a table for WCTI for air temperatures ranging from 10 to \(-60^{\circ} \mathrm{C}\) and wind speeds ranging from 10 to \(80 \mathrm{~km} / \mathrm{h}\). Comment on the magnitude of the cooling effect of the wind and the danger of frostbite.

What is the physical mechanism of heat conduction in a solid, a liquid, and a gas?

A 25 -cm-diameter black ball at \(130^{\circ} \mathrm{C}\) is suspended in air, and is losing heat to the surrounding air at \(25^{\circ} \mathrm{C}\) by convection with a heat transfer coefficient of \(12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and by radiation to the surrounding surfaces at \(15^{\circ} \mathrm{C}\). The total rate of heat transfer from the black ball is (a) \(217 \mathrm{~W}\) (b) \(247 \mathrm{~W}\) (c) \(251 \mathrm{~W}\) (d) \(465 \mathrm{~W}\) (e) \(2365 \mathrm{~W}\)

A flat-plate solar collector is used to heat water by having water flow through tubes attached at the back of the thin solar absorber plate. The absorber plate has a surface area of \(2 \mathrm{~m}^{2}\) with emissivity and absorptivity of \(0.9\). The surface temperature of the absorber is \(35^{\circ} \mathrm{C}\), and solar radiation is incident on the absorber at \(500 \mathrm{~W} / \mathrm{m}^{2}\) with a surrounding temperature of \(0^{\circ} \mathrm{C}\). Convection heat transfer coefficient at the absorber surface is \(5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), while the ambient temperature is \(25^{\circ} \mathrm{C}\). Net heat rate absorbed by the solar collector heats the water from an inlet temperature \(\left(T_{\text {in }}\right)\) to an outlet temperature \(\left(T_{\text {out }}\right)\). If the water flow rate is \(5 \mathrm{~g} / \mathrm{s}\) with a specific heat of \(4.2 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\), determine the temperature rise of the water.

The heat generated in the circuitry on the surface of a silicon chip \((k=130 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) is conducted to the ceramic substrate to which it is attached. The chip is \(6 \mathrm{~mm} \times 6 \mathrm{~mm}\) in size and \(0.5 \mathrm{~mm}\) thick and dissipates \(5 \mathrm{~W}\) of power. Disregarding any heat transfer through the \(0.5-\mathrm{mm}\) high side surfaces, determine the temperature difference between the front and back surfaces of the chip in steady operation.

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