8 Analytic Solutions II Rutten Rosseland Mean Opacity

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8. Analytic Solutions II • • Rutten: Rosseland Mean Opacity & Diffusion Approx Gray

8. Analytic Solutions II • • Rutten: Rosseland Mean Opacity & Diffusion Approx Gray atmosphere Limb darkening

Rosseland Mean Extinction: In order to recast the diffusion approximation into the familiar expression

Rosseland Mean Extinction: In order to recast the diffusion approximation into the familiar expression for the total flux F as a function of the geometrical radial temperature gradient d. T / dz, we use the Rosseland Mean Extinction coefficient: Where k. R(z) = a. R(z) / r(z). It averages the extinction similarly to the formula for combining parallel resistors: 1/R = 1/R 1 + 1/R 2 + … The extinction represents resistance to the photon flux which favours the more transparent spectral windows. The Planck function temperature sensitivity, d. Bn /d. T enters as a weighting function for the same reason. It produces larger flux from a given spatial temperature gradient at frequencies where it is large.

The total energy flow is now given by: Where u is the total energy

The total energy flow is now given by: Where u is the total energy density defined before u = (4 s / c) T 4. This diffusion equation is also called the radiation conduction equation. It says a negative temperature gradient is required to let net radiative flux diffuse outwards through a star by thermal absorptions and re-emissions with a mean free photon path l = 1/r k. R. In the solar interior l is only a few millimetres, making the optical depth from the surface tn ~ 1011, so the diffusion approximations are very accurate.

The Eddington Approximation Using the equations for J and K at large depth we

The Eddington Approximation Using the equations for J and K at large depth we get the First Eddington Approximation, often called the Eddington approximation Validity: It is exact for isotropic radiation. It is also exact, at any depth tn, when In(t, m) can be expanded in odd powers of m, with all even coefficients ai = 0 in This implies the Eddington approximation may hold for tn < 1, in contrast to the approximations at large depth and the diffusion equation which requires LTE and therefore only holds for tn > 1.

Why Do Gray Atmosphere • • • Opacity independent of frequency Only true gray

Why Do Gray Atmosphere • • • Opacity independent of frequency Only true gray opacity is electron scattering Demonstrates radiative equilibrium Can relate to more general/realistic situations Can get exact solution: test approximate numerical techniques • Can set exam questions…

The major assumption in the gray atmosphere is that the opacity is independent of

The major assumption in the gray atmosphere is that the opacity is independent of frequency: dkn / dn = 0. The ERT simplifies considerably since we can integrate over frequency. where We now assume: 1. Radiative equilibrium: 2. Atmosphere is in LTE: Total radiative flux is constant throughout atmosphere: d. F / dt = 0 Hence Sn(T) = Bn(T) and S(T) = B(T) A useful quantity relation is the frequency integrated Planck function:

Using the frequency integrated terms, the moment equations for the ERT now become: Radiative

Using the frequency integrated terms, the moment equations for the ERT now become: Radiative equilibrium implies the flux is constant throughout the atmosphere, so d. H / dt = 0, since H = F / 4. This then gives S(t) = J(t) and K(t) = H(t + q), since H(t) = H (constant) and q is a constant of integration. Using the Eddington approximation that J(t) = 3 K(t), we get:

Using the second Eddington approximation, J(t = 0) = 2 H, we get q

Using the second Eddington approximation, J(t = 0) = 2 H, we get q = 2/3, which gives the Milne-Eddington approximation for a gray atmosphere: since F = 4 H and S = J. Here F = (s/p)Teff 4. The exact solution is usually written as: where q(t) is the Hopf function which varies slowly with t.

Temperature Structure: Assuming LTE gives S(t) = B(t) = (s/p)T 4 and using the

Temperature Structure: Assuming LTE gives S(t) = B(t) = (s/p)T 4 and using the Milne-Eddington approx above, we get In the above we get Teff = T(t = 2/3) as it should. Limb Darkening: Using the Eddington_Barbier surface relation I(0, m) = S(t = m) gives I(0, m) = F(2 + 3 m), so the centre-to-limb variation for a gray star is: This gives I(0, 0) / I(0, 1) = 0. 4, which is in excellent agreement Solar limb darkening.