Consider a surface at \(0^{\circ} \mathrm{C}\) that may be assumed to be a blackbody in an environment at \(25^{\circ} \mathrm{C}\). If \(300 \mathrm{~W} / \mathrm{m}^{2}\) of radiation is incident on the surface, the radiosity of this black surface is (a) \(0 \mathrm{~W} / \mathrm{m}^{2}\) (b) \(15 \mathrm{~W} / \mathrm{m}^{2}\) (c) \(132 \mathrm{~W} / \mathrm{m}^{2}\) (d) \(300 \mathrm{~W} / \mathrm{m}^{2}\) (e) \(315 \mathrm{~W} / \mathrm{m}^{2}\)

Short Answer

Expert verified
Answer: (e) 315 W/m²

Step by step solution

01

Convert temperatures to Kelvin

To work with the Stefan-Boltzmann law, we need to convert our given temperatures to Kelvin. The formula to convert Celsius to Kelvin is K = °C + 273.15. Surface temperature: \(T_s = 0 + 273.15 = 273.15 \mathrm{~K}\) Environment temperature: \(T_e = 25 + 273.15 = 298.15 \mathrm{~K}\)
02

Calculate emitted radiation

Next, we will find the emitted radiation from the surface using the Stefan-Boltzmann law, which states that the power radiated per unit area is proportional to the fourth power of the temperature. The formula is: \(E = \sigma * T^4\) where \(\sigma\) is the Stefan-Boltzmann constant (\(\approx 5.67 \times 10^{-8} \mathrm{W m^{-2} K^{-4}}\)) and T is the surface temperature in Kelvin. For our surface: \(E = (5.67 \times 10^{-8}) \times (273.15)^4 \approx 315.04 \mathrm{~W/m^2}\)
03

Calculate reflected radiation

Since the surface is assumed to be a blackbody, it absorbs all incident radiation. Therefore, the reflected radiation is 0 W/m².
04

Calculate radiosity

Now that we have both the emitted and reflected radiation values, we can find the radiosity by adding them: \(R = E + Reflected Radiation\) \(R = 315.04 \mathrm{~W/m^2} + 0 \mathrm{~W/m^2} \approx 315 \mathrm{~W/m^2}\)
05

Choose the correct answer

From our calculations, the radiosity of the black surface is approximately 315 W/m², which corresponds to the answer: (e) \(315 \mathrm{~W/m^2}\)

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Key Concepts

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

Blackbody Radiation
Blackbody radiation is the theoretical concept of an ideal emitter and absorber of radiation that plays a foundation role in the study of thermal radiation. A blackbody absorbs all incoming light and does not reflect or transmit any, making it a perfect absorber. Moreover, it emits radiation at a maximum rate for its given temperature. An everyday example to help visualize blackbody radiation might be a heated piece of iron that glows red due to its temperature.

When an object is heated, it emits thermal radiation across a spectrum of wavelengths, but a blackbody does this in a characteristic way described by Planck's radiation law. The emitted radiation depends solely on the temperature of the blackbody – not on its shape or material composition. In the provided exercise, the surface is assumed to be a blackbody at 0°C – a simplification to make calculations feasible, but also an excellent gateway to understand how temperature affects radiation emission.
Stefan-Boltzmann Law
The Stefan-Boltzmann law is a fundamental principle in thermodynamics that relates the thermal radiation energy emitted by a blackbody to its temperature. Expressed mathematically, the energy emitted per unit surface area of a blackbody is proportional to the fourth power of the absolute temperature of the body. The formula for this law is expressed as:
\[E = \textstyle{\sigma} T^4\]
where \(E\) is the emitted radiation per unit area, \(\sigma\) is the Stefan-Boltzmann constant (\roughly 5.67×10−8 W m−2 K−4), and \(T\) is the absolute temperature of the body in Kelvin.

In the exercise, this law helps determine how much energy the surface at 0°C emits. This is a crucial step in finding the total radiosity—how much energy leaves the surface—given that we're assuming the surface in question is a blackbody, which simplifies the real-world complexities.
Thermal Radiation
Thermal radiation refers to the emission of electromagnetic waves from all objects that have a temperature above absolute zero. This radiation results from the thermal motion of charged particles in materials. The nature of this radiation is sometimes visible, like the red glow from a hot object, but often it's invisible infrared radiation. Unlike conduction and convection, thermal radiation does not require a medium and can even occur through the vacuum of space.

The amount and distribution of this emitted radiation depend on the temperature of the emitting body and its surface properties. In the case of the exercise solution, the surface emits thermal radiation as it is above absolute zero, but the calculation uses the idealized scenario where the surface emits thermal radiation as a blackbody would.
Heat Transfer
Heat transfer is a discipline in physics and engineering that deals with the movement of thermal energy from one place to another or from one object to another. This can happen in three main ways: conduction, where heat moves through a solid; convection, where heat is carried away by moving fluids like water or air; and radiation, which is the transfer of energy through electromagnetic waves.

Radiosity in the context of heat transfer describes the total amount of energy radiated away from a surface. It includes the body's own emitted radiation and any reflected environmental radiation. In our exercise scenario, the blackbody assumption means that all incident radiation is absorbed, so the radiosity is just the radiation emitted by the surface. By solving for radiosity, we're effectively looking at the total impact of heat transfer by radiation from the surface.

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Most popular questions from this chapter

Two very large parallel plates are maintained at uniform temperatures of \(T_{1}=600 \mathrm{~K}\) and \(T_{2}=400 \mathrm{~K}\) and have emissivities \(\varepsilon_{1}=0.5\) and \(\varepsilon_{2}=0.9\), respectively. Determine the net rate of radiation heat transfer between the two surfaces per unit area of the plates.

A car mechanic is working in a shop whose interior space is not heated. Comfort for the mechanic is provided by two radiant heaters that radiate heat at a total rate of \(4 \mathrm{~kJ} / \mathrm{s}\). About 5 percent of this heat strikes the mechanic directly. The shop and its surfaces can be assumed to be at the ambient temperature, and the emissivity and absorptivity of the mechanic can be taken to be \(0.95\) and the surface area to be \(1.8 \mathrm{~m}^{2}\). The mechanic is generating heat at a rate of \(350 \mathrm{~W}\), half of which is latent, and is wearing medium clothing with a thermal resistance of \(0.7 \mathrm{clo}\). Determine the lowest ambient temperature in which the mechanic can work comfortably.

Consider two concentric spheres forming an enclosure with diameters of \(12 \mathrm{~cm}\) and \(18 \mathrm{~cm}\) and surface temperatures \(300 \mathrm{~K}\) and \(500 \mathrm{~K}\), respectively. Assuming that the surfaces are black, the net radiation exchange between the two spheres is (a) \(21 \mathrm{~W}\) (b) \(140 \mathrm{~W}\) (c) \(160 \mathrm{~W}\) (d) \(1275 \mathrm{~W}\) (e) \(3084 \mathrm{~W}\)

Consider a person whose exposed surface area is \(1.9 \mathrm{~m}^{2}\), emissivity is \(0.85\), and surface temperature is \(30^{\circ} \mathrm{C}\). Determine the rate of heat loss from that person by radiation in a large room whose walls are at a temperature of (a) \(300 \mathrm{~K}\) and (b) \(280 \mathrm{~K}\).

What is latent heat? How is the latent heat loss from the human body affected by \((a)\) skin wettedness and \((b)\) relative humidity of the environment? How is the rate of evaporation from the body related to the rate of latent heat loss?

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