Stefan–Boltzmann law

With his law Stefan also determined the temperature of the Sun's surface.[8] He inferred from the data of Jacques-Louis Soret (1827–1890)[9] that the energy flux density from the Sun is 29 times greater than the energy flux density of a certain warmed metal lamella (a thin plate). A round lamella was placed at such a distance from the measuring device that it would be seen at the same angular diameter as the Sun. Soret estimated the temperature of the lamella to be approximately 1900 °C to 2000 °C. Stefan surmised that ⅓ of the energy flux from the Sun is absorbed by the Earth's atmosphere, so he took for the correct Sun's energy flux a value 3/2 times greater than Soret's value, namely 29 × 3/2 = 43.5.

Precise measurements of atmospheric absorption were not made until 1888 and 1904. The temperature Stefan obtained was a median value of previous ones, 1950 °C and the absolute thermodynamic one 2200 K. As 2.57⁴ = 43.5, it follows from the law that the temperature of the Sun is 2.57 times greater than the temperature of the lamella, so Stefan got a value of 5430 °C or 5700 K. This was the first sensible value for the temperature of the Sun. Before this, values ranging from as low as 1800 °C to as high as 13,000,000 °C[10] were claimed. The lower value of 1800 °C was determined by Claude Pouillet (1790–1868) in 1838 using the Dulong–Petit law.[11] Pouillet also took just half the value of the Sun's correct energy flux.

The temperature of stars other than the Sun can be approximated using a similar means by treating the emitted energy as a black body radiation.[12] So:

${\displaystyle L=4\pi R^{2}\sigma T^{4}}$

where L is the luminosity, σ is the Stefan–Boltzmann constant, R is the stellar radius and T is the effective temperature. This formula can then be rearranged to calculate the temperature:

${\displaystyle T={\sqrt[{4}]{\frac {L}{4\pi R^{2}\sigma }}}}$

or alternatively the radius:

${\displaystyle R={\sqrt {\frac {L}{4\pi \sigma T^{4}}}}}$

The same formulae can also be simplified to compute the parameters relative to the Sun:

${\displaystyle {\frac {L}{L_{\odot }}}=\left({\frac {R}{R_{\odot }}}\right)^{2}\left({\frac {T}{T_{\odot }}}\right)^{4}}$

${\displaystyle {\frac {T}{T_{\odot }}}=\left({\frac {L}{L_{\odot }}}\right)^{1/4}{\sqrt {\frac {R_{\odot }}{R}}}}$

${\displaystyle {\frac {R}{R_{\odot }}}=\left({\frac {T_{\odot }}{T}}\right)^{2}{\sqrt {\frac {L}{L_{\odot }}}}}$

where ${\displaystyle R_{\odot }}$ is the solar radius, and so forth. They can also be rewritten in terms of the surface area A and radiant emittance ${\displaystyle j^{\star }}$:

${\displaystyle L=Aj^{\star }}$

${\displaystyle j^{\star }={\frac {L}{A}}}$

${\displaystyle A={\frac {L}{j^{\star }}}}$

where ${\displaystyle A=4\pi R^{2}}$ and ${\displaystyle j^{\star }=\sigma T^{4}.}$

With the Stefan–Boltzmann law, astronomers can easily infer the radii of stars. The law is also met in the thermodynamics of black holes in so-called Hawking radiation.

Similarly we can calculate the effective temperature of the Earth T_⊕ by equating the energy received from the Sun and the energy radiated by the Earth, under the black-body approximation (Earth's own production of energy being small enough to be negligible). The luminosity of the Sun, L_⊙, is given by:

${\displaystyle L_{\odot }=4\pi R_{\odot }^{2}\sigma T_{\odot }^{4}}$

At Earth, this energy is passing through a sphere with a radius of a₀, the distance between the Earth and the Sun, and the irradiance (received power per unit area) is given by

${\displaystyle E_{\oplus }={\frac {L_{\odot }}{4\pi a_{0}^{2}}}}$

The Earth has a radius of R_⊕, and therefore has a cross-section of ${\displaystyle \pi R_{\oplus }^{2}}$. The radiant flux (i.e. solar power) absorbed by the Earth is thus given by:

${\displaystyle \Phi _{\text{abs}}=\pi R_{\oplus }^{2}\times E_{\oplus }:}$

Because the Stefan–Boltzmann law uses a fourth power, it has a stabilizing effect on the exchange and the flux emitted by Earth tends to be equal to the flux absorbed, close to the steady state where:

${\displaystyle {\begin{aligned}4\pi R_{\oplus }^{2}\sigma T_{\oplus }^{4}&=\pi R_{\oplus }^{2}\times E_{\oplus }\\&=\pi R_{\oplus }^{2}\times {\frac {4\pi R_{\odot }^{2}\sigma T_{\odot }^{4}}{4\pi a_{0}^{2}}}\\\end{aligned}}}$

T_⊕ can then be found:

${\displaystyle {\begin{aligned}T_{\oplus }^{4}&={\frac {R_{\odot }^{2}T_{\odot }^{4}}{4a_{0}^{2}}}\\T_{\oplus }&=T_{\odot }\times {\sqrt {\frac {R_{\odot }}{2a_{0}}}}\\&=5780\;{\rm {K}}\times {\sqrt {696\times 10^{6}\;{\rm {m}} \over 2\times 149.598\times 10^{9}\;{\rm {m}}}}\\&\approx 279\;{\rm {K}}\end{aligned}}}$

where T_⊙ is the temperature of the Sun, R_⊙ the radius of the Sun, and a₀ is the distance between the Earth and the Sun. This gives an effective temperature of 6 °C on the surface of the Earth, assuming that it perfectly absorbs all emission falling on it and has no atmosphere.

The Earth has an albedo of 0.3, meaning that 30% of the solar radiation that hits the planet gets scattered back into space without absorption. The effect of albedo on temperature can be approximated by assuming that the energy absorbed is multiplied by 0.7, but that the planet still radiates as a black body (the latter by definition of effective temperature, which is what we are calculating). This approximation reduces the temperature by a factor of 0.7^1/4, giving 255 K (−18 °C).[13][14]

The above temperature is Earth's as seen from space, not ground temperature but an average over all emitting bodies of Earth from surface to high altitude. Because of the greenhouse effect, the Earth's actual average surface temperature is about 288 K (15 °C), which is higher than the 255 K effective temperature, and even higher than the 279 K temperature that a black body would have.

In the above discussion, we have assumed that the whole surface of the earth is at one temperature. Another interesting question is to ask what the temperature of a blackbody surface on the earth would be assuming that it reaches equilibrium with the sunlight falling on it. This of course depends on the angle of the sun on the surface and on how much air the sunlight has gone through. When the sun is at the zenith and the surface is horizontal, the irradiance can be as high as 1120 W/m².[15] The Stefan–Boltzmann law then gives a temperature of

${\displaystyle T=\left({\frac {1120{\text{ W/m}}^{2}}{\sigma }}\right)^{1/4}\approx 375{\text{ K}}}$

or 102 °C. (Above the atmosphere, the result is even higher: 394 K.) We can think of the earth's surface as "trying" to reach equilibrium temperature during the day, but being cooled by the atmosphere, and "trying" to reach equilibrium with starlight and possibly moonlight at night, but being warmed by the atmosphere.

The fact that the energy density of the box containing radiation is proportional to ${\displaystyle T^{4}}$ can be derived using thermodynamics.[16][17] This derivation uses the relation between the radiation pressure p and the internal energy density ${\displaystyle u}$, a relation that can be shown using the form of the electromagnetic stress–energy tensor. This relation is:

${\displaystyle p={\frac {u}{3}}.}$

Now, from the fundamental thermodynamic relation

${\displaystyle dU=T\,dS-p\,dV,}$

we obtain the following expression, after dividing by ${\displaystyle dV}$ and fixing ${\displaystyle T}$ :

${\displaystyle \left({\frac {\partial U}{\partial V}}\right)_{T}=T\left({\frac {\partial S}{\partial V}}\right)_{T}-p=T\left({\frac {\partial p}{\partial T}}\right)_{V}-p.}$

The last equality comes from the following Maxwell relation:

${\displaystyle \left({\frac {\partial S}{\partial V}}\right)_{T}=\left({\frac {\partial p}{\partial T}}\right)_{V}.}$

From the definition of energy density it follows that

${\displaystyle U=uV}$

where the energy density of radiation only depends on the temperature, therefore

${\displaystyle \left({\frac {\partial U}{\partial V}}\right)_{T}=u\left({\frac {\partial V}{\partial V}}\right)_{T}=u.}$

Now, the equality

${\displaystyle \left({\frac {\partial U}{\partial V}}\right)_{T}=T\left({\frac {\partial p}{\partial T}}\right)_{V}-p,}$

after substitution of ${\displaystyle \left({\frac {\partial U}{\partial V}}\right)_{T}.}$ Meanwhile, the pressure is the rate of momentum change per unit area. Since the momentum of a photon is the same as the energy divided by the speed of light,

${\displaystyle u={\frac {T}{3}}\left({\frac {\partial u}{\partial T}}\right)_{V}-{\frac {u}{3}},}$

where the 1/3 factor comes from the projection of the momentum transfer onto the normal to the wall of the container.

Since the partial derivative ${\displaystyle \left({\frac {\partial u}{\partial T}}\right)_{V}}$ can be expressed as a relationship between only ${\displaystyle u}$ and ${\displaystyle T}$ (if one isolates it on one side of the equality), the partial derivative can be replaced by the ordinary derivative. After separating the differentials the equality becomes

${\displaystyle {\frac {du}{4u}}={\frac {dT}{T}},}$

which leads immediately to ${\displaystyle u=AT^{4}}$, with ${\displaystyle A}$ as some constant of integration.

Deriving the Stefan–Boltzmann Law using the Planck's law.

The law can be derived by considering a small flat black body surface radiating out into a half-sphere. This derivation uses spherical coordinates, with θ as the zenith angle and φ as the azimuthal angle; and the small flat blackbody surface lies on the xy-plane, where θ = ^π/₂.

The intensity of the light emitted from the blackbody surface is given by Planck's law :

$${\displaystyle I(\nu ,T)={\frac {2h\nu ^{3}}{c^{2}}}{\frac {1}{e^{h\nu /(kT)}-1}}.}$$

where

• ${\displaystyle I(\nu ,T)}$ is the amount of power per unit surface area per unit solid angle per unit frequency emitted at a frequency ${\displaystyle \nu }$ by a black body at temperature T.
• ${\displaystyle h}$ is Planck's constant
• ${\displaystyle c}$ is the speed of light, and
• ${\displaystyle k}$ is Boltzmann's constant.

The quantity ${\displaystyle I(\nu ,T)~A~d\nu ~d\Omega }$ is the power radiated by a surface of area A through a solid angle dΩ in the frequency range between ν and ν + dν.

The Stefan–Boltzmann law gives the power emitted per unit area of the emitting body,

$${\displaystyle {\frac {P}{A}}=\int _{0}^{\infty }I(\nu ,T)\,d\nu \int \cos \theta \,d\Omega }$$

Note that the cosine appears because black bodies are Lambertian (i.e. they obey Lambert's cosine law), meaning that the intensity observed along the sphere will be the actual intensity times the cosine of the zenith angle. To derive the Stefan–Boltzmann law, we must integrate ${\textstyle d\Omega =\sin \theta \,d\theta \,d\varphi }$ over the half-sphere and integrate ${\displaystyle \nu }$ from 0 to ∞.

$${\displaystyle {\begin{aligned}{\frac {P}{A}}&=\int _{0}^{\infty }I(\nu ,T)\,d\nu \int _{0}^{2\pi }\,d\varphi \int _{0}^{\pi /2}\cos \theta \sin \theta \,d\theta \\&=\pi \int _{0}^{\infty }I(\nu ,T)\,d\nu \end{aligned}}}$$

Then we plug in for I:

$${\displaystyle {\frac {P}{A}}={\frac {2\pi h}{c^{2}}}\int _{0}^{\infty }{\frac {\nu ^{3}}{e^{\frac {h\nu }{kT}}-1}}\,d\nu }$$

To evaluate this integral, do a substitution,

$${\displaystyle {\begin{aligned}u&={\frac {h\nu }{kT}}\\[6pt]du&={\frac {h}{kT}}\,d\nu \end{aligned}}}$$

which gives:

$${\displaystyle {\frac {P}{A}}={\frac {2\pi h}{c^{2}}}\left({\frac {kT}{h}}\right)^{4}\int _{0}^{\infty }{\frac {u^{3}}{e^{u}-1}}\,du.}$$

The integral on the right is standard and goes by many names: it is a particular case of a Bose–Einstein integral, the polylogarithm, or the Riemann zeta function ${\displaystyle \zeta (s)}$. The value of the integral is ${\displaystyle \Gamma (4)\zeta (4)={\frac {\pi ^{4}}{15}}}$ (where ${\displaystyle \Gamma (s)}$ is the Gamma function), giving the result that, for a perfect blackbody surface:

$${\displaystyle j^{\star }=\sigma T^{4}~,~~\sigma ={\frac {2\pi ^{5}k^{4}}{15c^{2}h^{3}}}={\frac {\pi ^{2}k^{4}}{60\hbar ^{3}c^{2}}}.}$$

Finally, this proof started out only considering a small flat surface. However, any differentiable surface can be approximated by a collection of small flat surfaces. So long as the geometry of the surface does not cause the blackbody to reabsorb its own radiation, the total energy radiated is just the sum of the energies radiated by each surface; and the total surface area is just the sum of the areas of each surface—so this law holds for all convex blackbodies, too, so long as the surface has the same temperature throughout. The law extends to radiation from non-convex bodies by using the fact that the convex hull of a black body radiates as though it were itself a black body.

The total energy density U can be similarly calculated, except the integration is over the whole sphere and there is no cosine, and the energy flux (U c) should be divided by the velocity c to give the energy density U:

$${\displaystyle U={\frac {1}{c}}\int _{0}^{\infty }I(\nu ,T)\,d\nu \int \,d\Omega }$$

Thus ${\textstyle \int _{0}^{\pi /2}\cos \theta \sin \theta \,d\theta }$ is replaced by ${\textstyle \int _{0}^{\pi }\sin \theta \,d\theta }$, giving an extra factor of 4.

Thus, in total:

$${\displaystyle U={\frac {4}{c}}\,\sigma \,T^{4}}$$