Chapter 8. Opacity

In this chapter we deal with the opacity $\kappa(\rho,T)$ [cm$^2$/g], which corresponds to the efficiency of energy transport via radiation.

In optically thick gas, energy is transported via photon diffusion. As is discussed in Chapter 5, we have

Fν=c3ρκνdeintdrF_\nu=-\frac{c}{3\rho\kappa_\nu}\frac{\text de_\text{int}}{\text dr}

where $e\text{int}$ is given by the blackbody radiation luminosity $B\nu$

eint=4πcBν(T)=8πhν3c31ehν/kBT1e_\text{int}=\frac{4\pi}cB_\nu(T)=\frac{8\pi h\nu^3}{c^3}\frac1{e^{h\nu/k_BT}-1}

Thus

Fν=4π3ρκνBνTTrF_\nu=-\frac{4\pi}{3\rho\kappa_\nu}\frac{\partial B_\nu}{\partial T}\frac{\partial T}{\partial r}

The total flux is

F=4ac3ρκRT3TrF=-\frac{4ac}{3\rho\kappa_R}T^3\frac{\partial T}{\partial r}

where $\kappa_R$ is the Rosseland mean opacity. Obviously, the efficiency of energy transported outward is inversely proportional to the opacity.

We can further define optical depth $\tau$,

τν=ρκνdrρκνr\tau_\nu=\int\rho\kappa_\nu\text dr\sim\rho\kappa_\nu r

So when $\tau\gg1$ so that energy is transported via photon diffusion, the flux is approximately

FacT4ρκrσSBT4τF\sim\frac{acT^4}{\rho\kappa r}\sim\frac{\sigma_{SB}T^4}{\tau}

Electron Scattering

If an electromagnetic wave passes an electron, the electric field makes the electron oscillate. The oscillating electron represents a classical dipole that radiates in other directions, i.e. the electron scatters part of the energy of the incoming waves.

From classical electrodynamics, elastic scattering of non-relativistic electrons, namely Thomson scattering, yields a cross section of

σT=8π3re2\sigma_T=\frac{8\pi}{3}{r_\text e^2}

where $r_\text e$ is the classical electron radius. Thus the opacity is

κνes=8π3re2μemp0.35 cm2/g\kappa^\text{es}_\nu=\frac{8\pi}{3}\frac{r_\text e^2}{\mu_em_\text p}\simeq0.35\text{ cm}^2\text{/g}

This opacity is $\nu$-independent, but when $T>10^8$ K, $\kappa\nu$ slightly decreases ($\sim20\%$ at $10^8$ K) for higher $T$. At that time the kinetic energy of electron is over $\sim10$ keV, $\gtrsim1\%$ of $m\text{e}c^2$. Therefore relativistic corrections (Compton scattering) become important.

Absorption Due to Free-free Transitions

If during its thermal motion a free electron passes an ion, the two charged particles form a system which can absorb and emit radiation. This mechanism is only effective as long as electron and ion are sufficiently close.

Let us first consider the emissivity $\varepsilon_\nu^\text{ff}$ [erg/s/cm$^3$/Hz]. In a super, super rough estimation, it should be proportional to the densities of both electron and ions, as well as the duration of the fly-by, which inversely proportional to the magnitude of their relative velocity.

ενffnenionv\varepsilon_\nu^\text{ff}\propto \frac{n_\text{e}n_\text{ion}}{|v|}

Assuming the thermal equilibrium, electrons obey the Boltzmann distribution, $|v|\propto T^{1/2}$. As a result,

ενffρ2T1/2\varepsilon_\nu^\text{ff}\propto \rho^2T^{-1/2}

Thus the opacity due to free-free transitions is

κνff=ανρ=ενffρBν(T)\kappa_\nu^\text{ff}=\frac{\alpha_\nu}{\rho}=\frac{\varepsilon_\nu^\text{ff}}{\rho B_\nu(T)}

The second equation is given by Kirchhoff's law of thermal radiation, which states that

For a body of any arbitrary material emitting and absorbing thermal electromagnetic radiation at every wavelength in thermodynamic equilibrium, the ratio of its emissive power to its dimensionless coefficient of absorption is equal to a universal function only of radiative wavelength and temperature. That universal function describes the perfect black-body emissive power.

And thus

Bν(T)=ενffανB_\nu(T)=\frac{\varepsilon_\nu^\text{ff}}{\alpha_\nu}

where the absorption coefficient $\alpha\nu\equiv\rho\kappa\nu$ [1/cm] denotes the attentuation of radiation per unit distance. So,

κνffρ1ενffν3ρT1/2ν3\kappa_\nu^\text{ff}\propto\rho^{-1}{\varepsilon^{\text{ff}}_\nu}\nu^{-3}\propto\rho T^{-1/2}\nu^{-3}

And the Rosseland mean opacity is

κff=Bν(T)Tdν1κνBν(T)TdνρT7/2\kappa^\text{ff}=\frac{\int\frac{\partial B_\nu(T)}{\partial T}\text d\nu}{\int\frac{1}{\kappa_\nu}\frac{\partial B_\nu(T)}{\partial T}\text d\nu}\propto\rho T^{-7/2}

This $\rho T^{-7/2}$ dependence is known as the Kramer's law. Precise derivation gives,

κff=4×1022(ρgcm3)(TK)7/2 cm2/g\kappa^\text{ff}=4\times10^{22}\left(\frac{\rho}{\text{g}\cdot\text{cm}^3}\right)\left(\frac{T}{\text K}\right)^{-7/2}\text{ cm}^2\text{/g}

Bound-free Transitions

The best-known example is ionization of atoms. For a hydrogen atom at its ground state, the ionization process is

Here the energy of $\gamma$ must be higher than 13.6 eV, otherwise this reaction will not occur. In other words, for $h\nuh\nu0$, $\alpha\nu\propto\nu^{-3}$. Different excitation states have different $\nu0$. The opacity $\kappa^\text{bf}{\nu}$ for a mixture of hydrogen atoms in different states of excitation is a superposition of $\alpha\nu$ for different stages of excitation. The resulting $\kappa^\text{bf}{\nu}$􏰁􏰂 is a sawtooth function.

The relative scale of $\kappa^\text{bf}{\nu}$ comparing to $\kappa^\text{ff}{\nu}$ is approximately

κνbf103Zκνbf\kappa^\text{bf}_{\nu}\simeq10^3Z\kappa^\text{bf}_{\nu}

where $Z$ is the metalicity. $Z_\odot\sim0.02$.

Bound-bound Transitions

$\kappa^\text{bb}_\nu$ is the superposition for opacity due to numerous possiblities of line adsorption. The dependency on $\nu$ is thus really messy.

The Negative Hydrogen Ion ($\ce{H-}$)

At a sufficiently low temperature, protons and electrons start to recombine. When it gets even cooler, $\ce{H-}$ begins to effectively form via

$\ce {H-}$ can also contribute to the opacity through photo-dissociation

With Saha equation, we can estimate the $\ce{H-}$ fraction as a function of temperature and density. Then we can obtain the Rosseland mean opacity

when $3000<T\text{ [K]}<6000$ and $10^{-10}<\rho \text{ [g/cm}^3]<10^{-5}$.

An Example: Stellar Pulsation

Consider that in an atmosphere, the energy is transported via radiation, then a small perturbation in the luminosity is given by

LT4κδLL=4δTTδκκL\propto\frac{T^4}{\kappa}\Rightarrow\frac{\delta L}{L}=4\frac{\delta T}{T}-\frac{\delta \kappa}{\kappa}

Define

κρlnκlnρT,κTlnκlnTρ\kappa_\rho\equiv\frac{\partial\ln\kappa}{\partial\ln \rho}\Bigg|_T,\quad \kappa_T\equiv\frac{\partial\ln\kappa}{\partial\ln T}\Bigg|_\rho

Then we have

δLL=(4κT)δTTκρδρρ\frac{\delta L}{L}=\left(4-\kappa_T\right)\frac{\delta T}{T}-\kappa_\rho\frac{\delta \rho}{\rho}

For simplicity, let us consider adiabatic perturbation for ideal gas

PρTρ5/3Tρ2/3δTT=23δρρP\propto\rho T\propto\rho^{5/3}\Rightarrow T\propto\rho^{2/3}\Rightarrow\frac{\delta T}T=\frac23\frac{\delta \rho}{\rho}

As a result,

δLL=(4κT32κρ)δTT\frac{\delta L}{L}=\left(4-\kappa_T-\frac32\kappa_\rho\right)\frac{\delta T}{T}
  • Case 1: $\kappa=\kappa^\text{es}\Rightarrow \kappa_\rho=0, \kappa_T=0$

    δLL=4δTT\Rightarrow\frac{\delta L}{L}=4\frac{\delta T}{T}

    When the temperature slightly increases, more energy will be radiated outwards within unit time. Thus the star is stable.

  • Case 2: $\kappa=\kappa^\text{ff}\Rightarrow \kappa_\rho=1, \kappa_T=-7/2$

    δLL=6δTT\Rightarrow\frac{\delta L}{L}=6\frac{\delta T}{T}

    Similarly, the star is stable.

  • Case 3: $\kappa=\kappa^\ce{H-}\Rightarrow \kappa_\rho=1/2, \kappa_T=9$

    δLL=234δTT\Rightarrow\frac{\delta L}{L}=-\frac{23}4\frac{\delta T}{T}

    The star is unstable and will excite pulsation. This happens for Cepheids, whose envelops are relatively cool.

In fact, given certain stellar mass and metallicity, each star has a $\log\kappa-\log T$ profile. The temperature regions with negative slope are vulnerable of pulsation.

Last updated