Unclear formula for radiative energy transfer

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SUMMARY

The discussion centers on the formula for radiative energy transfer, specifically the equation q = σ(T²⁴ - T¹⁴) / (1/ε₁ + 1/ε₂ - 1), which calculates heat flux density between two bodies with temperatures T₁ and T₂ and emissivity factors ε₁ and ε₂. Participants clarify that the equation applies to two surfaces facing each other with a narrow gap, emphasizing the importance of both emissivity and reflectivity in deriving the formula. The derivation involves understanding the heat flux contributions from both surfaces and solving for the net heat flux. The discussion concludes with an acknowledgment of the significance of surface properties in accurately applying the formula.

PREREQUISITES
  • Understanding of thermodynamics principles
  • Familiarity with the Stefan-Boltzmann law
  • Knowledge of emissivity and reflectivity concepts
  • Basic algebra for solving equations
NEXT STEPS
  • Study the derivation of the Stefan-Boltzmann law
  • Learn about emissivity and its impact on thermal radiation
  • Explore applications of radiative heat transfer in engineering
  • Investigate the effects of surface geometry on heat transfer
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Students in thermodynamics, engineers working with thermal systems, and researchers focusing on heat transfer applications will benefit from this discussion.

kontejnjer
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Right, so I was going over the formula sheet for my upcoming exam in thermodynamics, and I've stumbled upon this formula:

[itex]q=\frac{\sigma(T^{4}_{2}-T^{4}_{1})}{\frac{1}{\epsilon_1}+\frac{1}{\epsilon_2}-1}[/itex]

with a description that (I think) translates as heat flux density. I'm currently puzzled as to where this equation is applied, as our assistant didn't say anything about it or how it was derived in the first place.

I'm guessing that we have two bodies with temperatures [itex]T_1[/itex] and [itex]T_2[/itex] with emissivity factors [itex]\epsilon_1[/itex] and [itex]\epsilon_2[/itex], so q is supposed to be the energy (heat) transferred in unit time over a unit surface from one body to the other, but I still haven't the slightest idea as to how this equation is derived. Are the shape of the bodies and their mutual position relevant here? What are the conditions under which the equation is applicable?

I'm somewhat puzzled so any help would be much appreciated.
 
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That's the formula for the heat flux Q between two surfaces at different temperatures T1 and T2 facing each other with a narrow gap in between (narrow enough that all the heat coming from one reaches the other).

To understand that equation you must realize that the surface 1 not only produces a heat flux Q1'=σε1T14, but also reflects a heat flux Q1''=(1-ε1)Q2, where Q2 is the heat coming from surface 2 and (1-ε1) is surface 1's albedo. So we get

Q1 = Q1' + Q1'' = σε1T14 + (1-ε1)Q2

and a similar equation for Q2. Solve those equations for Q1 and Q2 and finally subtract them to find Q = Q1 - Q2 to find the net heat flux, and if all goes well, you should get to your mystery equation.
 
Last edited:
Ahh, I see it now, I completely forgot about the reflectivity of both surfaces so my original derivation didn't match up, thanks a lot!
 

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