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Two parallel disks of diameter \(D=0.6 \mathrm{~m}\) separated by \(L=0.4 \mathrm{~m}\) are located directly on top of each other. Both disks are black and are maintained at a temperature of \(450 \mathrm{~K}\). The back sides of the disks are insulated, and the environment that the disks are in can be considered to be a blackbody at \(300 \mathrm{~K}\). Determine the net rate of radiation heat transfer from the disks to the environment.

Short Answer

Expert verified
According to the information provided and the solutions outlined in the steps above, please follow these calculations: Step 2: Calculate the radiative heat flux from the disks \(q_1 = (1)(5.67 \times 10^{-8}\ \mathrm{W/m^2K^4})(450 \mathrm{~K})^4 = 4010.1\ \mathrm{W/m^2}\) Step 3: Calculate the radiative heat flux returning to the disks from the environment \(q_2 = (1)(5.67 \times 10^{-8}\ \mathrm{W/m^2K^4})(300 \mathrm{~K})^4 = 459.3\ \mathrm{W/m^2}\) Step 4: Calculate the net rate of radiation heat transfer from the disks to the environment First, calculate the area of one disk: \(A = \pi (\frac{0.6}{2})^2 = \pi(0.3)^2 = 0.2827\ \mathrm{m^2}\) Now, calculate the net rate: \(q_{net} = 2A(q_1 - q_2) = 2(0.2827\ \mathrm{m^2}) (4010.1\ \mathrm{W/m^2} - 459.3\ \mathrm{W/m^2}) = 2 \times 0.2827 \times 3550.8\ \mathrm{W/m^2} = 2006.6\ \mathrm{W}\) Thus, the net rate of radiation heat transfer from the disks to the environment is 2006.6 W.

Step by step solution

01

Define the variables

The diameter of the disks is \(D=0.6 \mathrm{~m}\), the separation between the disks is \(L=0.4 \mathrm{~m}\), the temperature of the disks is \(T_1 = 450 \mathrm{~K}\), and the temperature of the environment is \(T_2 = 300 \mathrm{~K}\). We also know that both disks are black, and thus have the emissivity value \(\epsilon = 1\).
02

Calculate the radiative heat flux from the disks

Since the disks are black, we can use the Stefan-Boltzmann Law to determine the radiative heat flux emitted by the disks. The formula to find the radiative heat flux is: \(q = \epsilon \sigma T^4\) where \(\epsilon\) is the emissivity, \(\sigma\) is the Stefan-Boltzmann constant, which is equal to \(5.67 \times 10^{-8}\ \mathrm{W/m^2K^4}\), and \(T\) is the temperature in Kelvin. For each disk, the radiative heat flux emitted is: \(q_1 = \epsilon_1 \sigma T_1^4\) \(q_1 = (1)(5.67 \times 10^{-8}\ \mathrm{W/m^2K^4})(450 \mathrm{~K})^4\) Calculate \(q_1\).
03

Calculate the radiative heat flux returning to the disks from the environment

We also need to determine the radiative heat flux that comes back to the disks from the environment. The radiative heat flux from the environment returning to the disks is governed by its temperature \(T_2\). Using the same formula, we have: \(q_2 = \epsilon_2 \sigma T_2^4\) \(q_2 = (1)(5.67 \times 10^{-8}\ \mathrm{W/m^2K^4})(300 \mathrm{~K})^4\) Calculate \(q_2\).
04

Calculate the net rate of radiation heat transfer from the disks to the environment

To find the net rate of radiation heat transfer from the disks to the environment, we can subtract the radiative heat flux returning to the disks from the total radiative heat flux emitted by the disks. We also need to account for both disks, so we multiply the net flux by 2 and by the area of one disk, \(A\). The formula for the area of a disk is: \(A = \pi (\frac{D}{2})^2\) Calculate \(A\). Now, we can calculate the net rate like this: \(q_{net} = 2A(q_1 - q_2)\) Plug the values of \(A\), \(q_1\), and \(q_2\) into the formula and calculate the net rate of radiation heat transfer from the disks to the environment.

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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 fundamental in understanding radiation heat transfer. It relates the amount of energy radiated from a black body in terms of its temperature. Specifically, it states that the energy radiated per unit surface area of a black body is directly proportional to the fourth power of the black body's absolute temperature.

Mathematically, the law is expressed as:
\[ q = \.\epsilon \sigma T^4 \]
where \( q \) is the total radiated energy per unit area, \( \.\epsilon \) is the emissivity of the material, \( \sigma \) is the Stefan-Boltzmann constant (\( 5.67 \times 10^{-8} \mathrm{W/m^2K^4} \)), and \( T \) is the absolute temperature in kelvin.

This law is crucial for calculating the radiative heat transfer between objects and their surroundings, and for the design of systems where such transfer is significant, such as thermal insulation materials, radiators, and solar panels.
Emissivity
Emissivity is a measure of an object's ability to emit infrared energy compared to that of an ideal emitter, known as a black body. It is dimensionless and ranges from 0 to 1, where 1 corresponds to a perfect black body that emits the maximum amount of radiation possible at a given temperature, and 0 corresponds to a perfect reflector that emits no thermal radiation.

Factors Affecting Emissivity


The emissivity of a material can depend on several factors, such as:
  • Temperature: Some materials change their emissivity with temperature.
  • Surface roughness: Rougher surfaces tend to have higher emissivity.
  • Material composition: Different materials inherently have different emissivity values.
  • Surface coatings: Coatings can be applied to alter a material's emissivity.

In practical applications, engineers must consider the emissivity of materials when designing systems and predicting heat transfer rates, as it directly affects the Stefan-Boltzmann Law calculations.
Blackbody Radiation
Blackbody radiation is the thermal electromagnetic radiation emitted by an object that is an ideal emitter at all wavelengths. The term 'black body' might seem counterintuitive, but it signifies that the object absorbs all incident radiation, regardless of frequency or angle of incidence, which means it also emits the maximum amount of radiation possible.

A perfect black body with an emissivity of 1 is a theoretical concept, as all real objects have emissivities less than 1. Blackbody radiation forms the basis of the field of thermal radiation and is characterized by a spectrum dependent solely on the body's temperature, as described by the Planck's law.

Importance in Heat Transfer


Understanding blackbody radiation is fundamental for thermography, the development of infrared sensors, and in astrophysics, for studying the thermal properties of stars and planets. Moreover, calculating the net radiative heat transfer, as given in the original exercise, requires considering both the emission from the object and the absorption of blackbody radiation from its environment.

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Most popular questions from this chapter

A cylindrical container whose height and diameter are \(8 \mathrm{~m}\) is filled with a mixture of \(\mathrm{CO}_{2}\) and \(\mathrm{N}_{2}\) gases at \(600 \mathrm{~K}\) and \(1 \mathrm{~atm}\). The partial pressure of \(\mathrm{CO}_{2}\) in the mixture is \(0.15 \mathrm{~atm}\). If the walls are black at a temperature of \(450 \mathrm{~K}\), determine the rate of radiation heat transfer between the gas and the container walls.

Consider a 20-cm-diameter hemispherical enclosure. The dome is maintained at \(600 \mathrm{~K}\) and heat is supplied from the dome at a rate of \(50 \mathrm{~W}\) while the base surface with an emissivity of \(0.55\) is maintained at \(400 \mathrm{~K}\). Determine the emissivity of the dome.

Two very large parallel plates are maintained at uniform temperatures \(T_{1}=750 \mathrm{~K}\) and \(T_{2}=500 \mathrm{~K}\) and have emissivities \(\varepsilon_{1}=0.85\) and \(\varepsilon_{2}=0.7\), respectively. If a thin aluminum sheet with the same emissivity on both sides is to be placed between the plates in order to reduce the net rate of radiation heat transfer between the plates by 90 percent, the emissivity of the aluminum sheet must be (a) \(0.07\) (b) \(0.10\) (c) \(0.13\) (d) \(0.16\) (e) \(0.19\)

How can you determine the view factor \(F_{12}\) when the view factor \(F_{21}\) and the surface areas are available?

A 2-m-internal-diameter double-walled spherical tank is used to store iced water at \(0^{\circ} \mathrm{C}\). Each wall is \(0.5 \mathrm{~cm}\) thick, and the \(1.5\)-cm-thick air space between the two walls of the tank is evacuated in order to minimize heat transfer. The surfaces surrounding the evacuated space are polished so that each surface has an emissivity of \(0.15\). The temperature of the outer wall of the tank is measured to be \(20^{\circ} \mathrm{C}\). Assuming the inner wall of the steel tank to be at \(0^{\circ} \mathrm{C}\), determine \((a)\) the rate of heat transfer to the iced water in the tank and \((b)\) the amount of ice at \(0^{\circ} \mathrm{C}\) that melts during a 24-h period.

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