Abramowicz, M. A., & Fragile, P. C. (2013). Foundations of black hole accretion disk theory. Living Reviews in Relativity , 16 (1), Article 1. https://doi.org/10.12942/lrr-2013-1
Parameters
Parameters
Expression
total mass
M ∗ M_* M ∗
total angular momentum
J ∗ J_* J ∗
rescaled mass
M = G M ∗ c 2 M=\dfrac{GM_*}{c^2} M = c 2 G M ∗
rescaled angular momentum
a = J ∗ M ∗ c a=\dfrac{J_*}{M_* c} a = M ∗ c J ∗
relative thickness
h = H R h=\dfrac{H}{R} h = R H
dimensionless accretion rate
m ˙ = 0.1 M ˙ c 2 L Edd \dot{m}=\dfrac{0.1\dot{M}c^2}{L_\text{Edd}} m ˙ = L Edd 0.1 M ˙ c 2
optical depth
τ \tau τ
importance of advection
q = Q adv Q rad q=\dfrac{Q_\text{adv}}{Q_\text{rad}} q = Q rad Q adv where Q Q Q represents an energy flux
importance of radiation pressure
β = P gas P gas + P rad \beta=\dfrac{P_\text{gas}}{P_\text{gas}+P_\text{rad}} β = P gas + P rad P gas
location of inner edge
r in r_\text{in} r in
accretion efficiency
η \eta η
marginally stable orbit (innermost stable circular orbit)
r ms r_\text{ms} r ms
marginally bound orbit
r mb r_\text{mb} r mb
energy
E ≡ − η μ p μ = − p t \mathcal{E}\equiv-\eta^\mu p_\mu=-p_t E ≡ − η μ p μ = − p t
angular momentum
L ≡ ξ μ p μ = p ϕ \mathcal{L}\equiv\xi^\mu p_\mu=p_\phi L ≡ ξ μ p μ = p ϕ
specific angular momentum
ℓ ≡ L E = − p ϕ p t = − u ϕ u t \ell\equiv\dfrac{\mathcal{L}}{\mathcal{E}}=-\dfrac{p_\phi}{p_t}=-\dfrac{u_\phi}{u_t} ℓ ≡ E L = − p t p ϕ = − u t u ϕ
angular velocity measured by ZAVO (Zero Angular Velocity Observer)
Ω = u ϕ u t = d ϕ d t \Omega=\dfrac{u^\phi}{u^t}=\dfrac{\mathrm{d}\phi}{\mathrm{d}t} Ω = u t u ϕ = d t d ϕ
redshift factor
A = u t A=u^t A = u t , − A − 2 = g t t + 2 Ω g t ϕ + Ω 2 g ϕ ϕ -A^{-2}=g_{tt}+2\Omega g_{t\phi}+\Omega^2 g_{\phi\phi} − A − 2 = g tt + 2Ω g tϕ + Ω 2 g ϕϕ
There are 4 types of accretion disks:
Thick Diskh > 1 , m ˙ ≫ 1 , τ ≫ 1 , q ∼ 1 , β ≪ 1 , r in ∼ r mb , η ≪ 0.1 h>1,\dot{m}\gg1,\tau\gg1,q\sim1,\beta\ll1,r_\text{in}\sim r_\text{mb},\eta\ll0.1
h > 1 , m ˙ ≫ 1 , τ ≫ 1 , q ∼ 1 , β ≪ 1 , r in ∼ r mb , η ≪ 0.1
Thin Diskh ≪ 1 , m ˙ < 1 , τ ≫ 1 , q = 0 , β ∼ 1 , r in = r ms , η ∼ 0.1 h\ll1,\dot{m}<1,\tau\gg1,q=0,\beta\sim1,r_\text{in}=r_\text{ms},\eta\sim0.1
h ≪ 1 , m ˙ < 1 , τ ≫ 1 , q = 0 , β ∼ 1 , r in = r ms , η ∼ 0.1
Slim Diskh ∼ 1 , m ˙ ⪆ 1 , τ ≫ 1 , q ∼ 1 , β < 1 , r mb < r in < r ms , η < 0.1 h\sim1,\dot{m}\gtrapprox1,\tau\gg1,q\sim1,\beta<1,r_\text{mb}<r_\text{in}<r_\text{ms},\eta<0.1
h ∼ 1 , m ˙ ⪆ 1 , τ ≫ 1 , q ∼ 1 , β < 1 , r mb < r in < r ms , η < 0.1
Advection-Dominated Accretion Flow (ADAF)h < 1 , m ˙ ≪ 1 , τ ≪ 1 , q ∼ 1 , β = 1 , r mb < r in < r ms , η ≪ 0.1 h<1,\dot{m}\ll1,\tau\ll1,q\sim1,\beta=1,r_\text{mb}<r_\text{in}<r_\text{ms},\eta\ll0.1
h < 1 , m ˙ ≪ 1 , τ ≪ 1 , q ∼ 1 , β = 1 , r mb < r in < r ms , η ≪ 0.1
General Principles
The fundamental conservation laws that govern the behavior of all matter, namely the conservation of rest mass and conservation of energy-momentum
∇ μ ( ρ u μ ) = 0 , ∇ μ T ν μ = 0. \nabla_\mu(\rho u^\mu)=0,\quad \nabla_\mu T_\nu^\mu=0.
∇ μ ( ρ u μ ) = 0 , ∇ μ T ν μ = 0.
Here ρ \rho ρ is the rest mass density, u μ u^\mu u μ is the four velocity of matter, and T ν μ T_\nu^\mu T ν μ is the stress energy tensor which can be written as,
( T ν μ ) GEN = ( T ν μ ) FLU + ( T ν μ ) VIS + ( T ν μ ) MAX + ( T ν μ ) RAD , ( T ν μ ) FLU = ( ρ u μ ) ( W u ν ) + δ ν μ P , ( T ν μ ) VIS = ν ∗ σ ν μ , ( T ν μ ) MAX = F μ α F α ν − 1 4 δ ν μ F α β F α β , ( T ν μ ) RAD = 4 3 E u μ u ν + u μ F ν + u ν F μ , \begin{aligned}
(T_\nu^\mu)_\text{GEN}&=(T_\nu^\mu)_\text{FLU}+(T_\nu^\mu)_\text{VIS}+(T_\nu^\mu)_\text{MAX}+(T_\nu^\mu)_\text{RAD}, \\
(T_\nu^\mu)_\text{FLU}&=(\rho u^\mu)(Wu_\nu)+\delta_\nu^\mu P, \\
(T_\nu^\mu)_\text{VIS}&=\nu_*\sigma_\nu^\mu, \\
(T_\nu^\mu)_\text{MAX}&=F^{\mu\alpha}F_{\alpha\nu}-\frac{1}{4}\delta_\nu^\mu F_{\alpha\beta}F^{\alpha\beta}, \\
(T_\nu^\mu)_\text{RAD}&=\frac{4}{3}Eu^\mu u_\nu+u^\mu F_\nu+u_\nu F^\mu,
\end{aligned}
( T ν μ ) GEN ( T ν μ ) FLU ( T ν μ ) VIS ( T ν μ ) MAX ( T ν μ ) RAD = ( T ν μ ) FLU + ( T ν μ ) VIS + ( T ν μ ) MAX + ( T ν μ ) RAD , = ( ρ u μ ) ( W u ν ) + δ ν μ P , = ν ∗ σ ν μ , = F μα F α ν − 4 1 δ ν μ F α β F α β , = 3 4 E u μ u ν + u μ F ν + u ν F μ ,
Here W W W is enthalpy, δ ν μ \delta_\nu^\mu δ ν μ is Kronecker delta tensor, P P P is pressure, ν ∗ \nu_* ν ∗ is kinematic viscosity, σ ν μ \sigma_\nu^\mu σ ν μ is shear, F μ ν F^{\mu\nu} F μν is Faraday electromagnetic field tensor, E E E is radiation energy density and F μ F^\mu F μ is radiation flux.
Thick Disks
Polish doughnuts
( T ν μ ) VIS = ( T ν μ ) MAX = ( T ν μ ) RAD = 0 (T_\nu^\mu)_\text{VIS}=(T_\nu^\mu)_\text{MAX}=(T_\nu^\mu)_\text{RAD}=0 ( T ν μ ) VIS = ( T ν μ ) MAX = ( T ν μ ) RAD = 0
assume for the stress energy tensor and four velocity,T ν μ = ( T ν μ ) FLU = ρ W u μ u ν + P δ ν μ , u μ = A ( η μ + Ω ξ μ ) , \begin{aligned}
T_\nu^\mu=(T_\nu^\mu)_\text{FLU}&=\rho Wu^\mu u_\nu+P\delta_\nu^\mu, \\
u^\mu&=A(\eta^\mu+\Omega\xi^\mu),
\end{aligned}
T ν μ = ( T ν μ ) FLU u μ = ρ W u μ u ν + P δ ν μ , = A ( η μ + Ω ξ μ ) ,
the equation for the equipressure surfaces, P ( r , θ ) = const P(r,\theta)=\text{const} P ( r , θ ) = const , may be written as r P ( θ ) r_P(\theta) r P ( θ ) with the function r P ( θ ) r_P(\theta) r P ( θ ) given by− d r P d θ = ∂ θ P ∂ r P = ( 1 − ℓ Ω ) ∂ θ ln A + ℓ ∂ θ Ω ( 1 − ℓ Ω ) ∂ r ln A + ℓ ∂ r Ω . -\frac{\mathrm{d}r_P}{\mathrm{d}\theta}=\frac{\partial_\theta P}{\partial_r P}=\frac{(1-\ell\Omega)\partial_\theta\ln A+\ell\partial_\theta\Omega}{(1-\ell\Omega)\partial_r\ln A+\ell\partial_r\Omega}.
− d θ d r P = ∂ r P ∂ θ P = ( 1 − ℓ Ω ) ∂ r ln A + ℓ ∂ r Ω ( 1 − ℓ Ω ) ∂ θ ln A + ℓ ∂ θ Ω .
Thin Disks
Equations in the Kerr geometry
Mass conservation (continuity)
Radial momentum conservation
Angular momentum conservation
Vertical equilibrium
Energy conservation
The eigenvalue problem
The thin disk equations can be reduced to a set of two ordinary differential equations for two dependent variables, e.g., the Mach number M = − V / c S = − V Σ / P \mathcal{M}=-V/c_S=-V\Sigma/P M = − V / c S = − V Σ/ P and the angular momentum L = u ϕ \mathcal{L}=u_\phi L = u ϕ
d ln M d ln r = N 1 ( r , M , L ) D ( r M , L ) d ln L d ln r = N 2 ( r , M , L ) D ( r M , L ) \frac{\mathrm{d}\ln\mathcal{M}}{\mathrm{d}\ln r}=\frac{\mathcal{N}_1(r,\mathcal{M},\mathcal{L})}{\mathcal{D}(r\mathcal{M},\mathcal{L})}\frac{\mathrm{d}\ln\mathcal{L}}{\mathrm{d}\ln r}=\frac{\mathcal{N}_2(r,\mathcal{M},\mathcal{L})}{\mathcal{D}(r\mathcal{M},\mathcal{L})}
d ln r d ln M = D ( r M , L ) N 1 ( r , M , L ) d ln r d ln L = D ( r M , L ) N 2 ( r , M , L )
At the “sonic” point ( D ( r , M , L ) = 0 \mathcal{D}(r,\mathcal{M},\mathcal{L})=0 D ( r , M , L ) = 0 ) r sonic r_\text{sonic} r sonic , the extra regularity conditions N i ( r , M , L ) = 0 \mathcal{N}_i(r,\mathcal{M},\mathcal{L})=0 N i ( r , M , L ) = 0 are satisfied only for one particular value L in \mathcal{L}_\text{in} L in , which is the eigenvalue of the problem.
Solutions
Using a more general scaling: m = M / M ⊙ m=M/M_\odot m = M / M ⊙ and m ˙ = M ˙ c 2 / L Edd \dot{m}=\dot{M}c^2/L_\text{Edd} m ˙ = M ˙ c 2 / L Edd .
Outer region: P = P gas P=P_\text{gas} P = P gas , κ = κ ff \kappa=\kappa_\text{ff} κ = κ ff (free-free opacity)F = [ 7 × 10 26 erg cm − 2 s − 1 ] ( m − 1 m ˙ ) r ∗ − 3 B − 1 C − 1 / 2 Q , Σ = [ 4 × 10 5 g cm − 2 ] ( α − 4 / 5 m 2 / 10 m ˙ 0 ∗ 7 / 10 ) r ∗ − 3 / 4 A 1 / 10 B − 4 / 5 C 1 / 2 D − 17 / 20 E − 1 / 20 Q 7 / 10 , H = [ 4 × 10 2 cm ] ( α − 1 / 10 m 18 / 20 m ˙ 3 / 20 ) r ∗ 9 / 8 A 19 / 20 B − 11 / 10 C 1 / 2 D − 23 / 40 E − 19 / 40 Q 3 / 20 , ρ 0 = [ 4 × 10 2 g cm − 3 ] ( α − 7 / 10 m − 7 / 10 m ˙ 11 / 20 ) r ∗ − 15 / 8 A − 17 / 20 B 3 / 10 D − 11 / 40 E 17 / 40 Q 11 / 20 , T = [ 2 × 10 8 K ] ( α − 1 / 5 m − 1 / 5 m ˙ 3 / 10 ) r ∗ − 3 / 4 A − 1 / 10 B − 1 / 5 D − 3 / 20 E 1 / 20 Q 3 / 10 , β / ( 1 − β ) = [ 3 ] ( α − 1 / 10 m − 1 / 10 m ˙ − 7 / 20 ) r ∗ 3 / 8 A − 11 / 20 B 9 / 10 D 7 / 40 E 11 / 40 Q − 7 / 20 , τ f f / τ e s = [ 2 × 10 − 3 ] ( m ˙ − 1 / 2 ) r ∗ 3 / 4 A − 1 / 2 B 2 / 5 D 1 / 4 E 1 / 4 Q − 1 / 2 , \begin{aligned}
F &= [7 \times 10^{26} \text{ erg~cm}^{-2}~\text{s}^{-1}](m^{-1} \dot{m})\,r^{-3}_*\, \mathcal{B}^{-1} \mathcal{C}^{-1/2} \mathcal{Q}, \\
\Sigma &= [4 \times 10^5 \text{ g~cm}^{-2}] (\alpha^{-4/5}\,m^{2/10} \dot{m}^{7/10}_{0*})\,r^{-3/4}_*\, \mathcal{A}^{1/10} \mathcal{B}^{-4/5} \mathcal{C}^{1/2} \mathcal{D}^{-17/20} \mathcal{E}^{-1/20} \mathcal{Q}^{7/10}, \\
H &= [4 \times 10^2 \text{ cm}] (\alpha^{-1/10}\,m^{18/20} \dot{m}^{3/20})\,r^{9/8}_* \,\mathcal{A}^{19/20} \mathcal{B}^{-11/10} \mathcal{C}^{1/2} \mathcal{D}^{-23/40} \mathcal{E}^{-19/40} \mathcal{Q}^{3/20}, \\
\rho_0 &= [4 \times 10^2 \text{ g~cm}^{-3}] (\alpha^{-7/10}\,m^{-7/10} \dot{m}^{11/20})\,r^{-15/8}_* \,\mathcal{A}^{-17/20} \mathcal{B}^{3/10} \mathcal{D}^{-11/40} \mathcal{E}^{17/40} \mathcal{Q}^{11/20}, \\
T &= [2 \times 10^8 \text{ K}] (\alpha^{-1/5}\,m^{-1/5} \dot{m}^{3/10})\,r^{-3/4}_*\, \mathcal{A}^{-1/10} \mathcal{B}^{-1/5} \mathcal{D}^{-3/20} \mathcal{E}^{1/20} \mathcal{Q}^{3/10}, \\
\beta/(1-\beta) &= [3](\alpha^{-1/10}\,m^{-1/10} \dot{m}^{-7/20})\,r^{3/8}_*\,\mathcal{A}^{-11/20} \mathcal{B}^{9/10} \mathcal{D}^{7/40} \mathcal{E}^{11/40} \mathcal{Q}^{-7/20}, \\
\tau_{ff}/{\tau}_{es} &= [2 \times 10^{-3}](\dot{m}^{-1/2})\,r^{3/4}_*\,\mathcal{A}^{-1/2} \mathcal{B}^{2/5} \mathcal{D}^{1/4} \mathcal{E}^{1/4} \mathcal{Q}^{-1/2},
\end{aligned}
F Σ H ρ 0 T β / ( 1 − β ) τ f f / τ es = [ 7 × 1 0 26 erg cm − 2 s − 1 ] ( m − 1 m ˙ ) r ∗ − 3 B − 1 C − 1/2 Q , = [ 4 × 1 0 5 g cm − 2 ] ( α − 4/5 m 2/10 m ˙ 0 ∗ 7/10 ) r ∗ − 3/4 A 1/10 B − 4/5 C 1/2 D − 17/20 E − 1/20 Q 7/10 , = [ 4 × 1 0 2 cm ] ( α − 1/10 m 18/20 m ˙ 3/20 ) r ∗ 9/8 A 19/20 B − 11/10 C 1/2 D − 23/40 E − 19/40 Q 3/20 , = [ 4 × 1 0 2 g cm − 3 ] ( α − 7/10 m − 7/10 m ˙ 11/20 ) r ∗ − 15/8 A − 17/20 B 3/10 D − 11/40 E 17/40 Q 11/20 , = [ 2 × 1 0 8 K ] ( α − 1/5 m − 1/5 m ˙ 3/10 ) r ∗ − 3/4 A − 1/10 B − 1/5 D − 3/20 E 1/20 Q 3/10 , = [ 3 ] ( α − 1/10 m − 1/10 m ˙ − 7/20 ) r ∗ 3/8 A − 11/20 B 9/10 D 7/40 E 11/40 Q − 7/20 , = [ 2 × 1 0 − 3 ] ( m ˙ − 1/2 ) r ∗ 3/4 A − 1/2 B 2/5 D 1/4 E 1/4 Q − 1/2 ,
where r ∗ = r c 2 / G M r_*=rc^2/GM r ∗ = r c 2 / GM .
Middle region: P = P gas P=P_\text{gas} P = P gas , κ = κ es \kappa=\kappa_\text{es} κ = κ es (electron-scattering opacity)F = [ 7 × 10 26 erg cm − 2 s − 1 ] ( m − 1 m ˙ ) r ∗ − 3 B − 1 C − 1 / 2 Q , Σ = [ 9 × 10 4 g cm − 2 ] ( α − 4 / 5 m 1 / 5 m ˙ 3 / 5 ) r ∗ − 3 / 5 B − 4 / 5 C 1 / 2 D − 4 / 5 Q 3 / 5 , H = [ 1 × 10 3 cm ] ( α − 1 / 10 m 9 / 10 m ˙ 1 / 5 ) r ∗ 21 / 20 A B − 6 / 5 C 1 / 2 D − 3 / 5 E − 1 / 2 Q 1 / 5 , ρ 0 = [ 4 × 10 1 g cm − 3 ] ( α − 7 / 10 m − 7 / 10 m ˙ 2 / 5 ) r ∗ − 33 / 20 A − 1 B 3 / 5 D − 1 / 5 E 1 / 2 Q 2 / 5 , T = [ 7 × 10 8 K ] ( α − 1 / 5 m − 1 / 5 m ˙ 2 / 5 ) r ∗ − 9 / 10 B − 2 / 5 D − 1 / 5 Q 2 / 5 , β / ( 1 − β ) = [ 7 × 10 − 3 ] ( α − 1 / 10 m − 1 / 10 m ˙ − 4 / 5 ) r ∗ 21 / 20 A − 1 B 9 / 5 D 2 / 5 E 1 / 2 Q − 4 / 5 , τ f f / τ e s = [ 2 × 10 − 6 ] ( m ˙ − 1 ) r ∗ 3 / 2 A − 1 B 2 D 1 / 2 E 1 / 2 Q − 1 , \begin{aligned}
F &= [7 \times 10^{26} \text{ erg~cm}^{-2}~\text{s}^{-1}](m^{-1} \dot{m})\,r^{-3}_*\, \mathcal{B}^{-1} \mathcal{C}^{-1/2} \mathcal{Q}, \\
\Sigma &= [9 \times 10^4 \text{ g~cm}^{-2}](\alpha^{-4/5} m^{1/5} \dot{m}^{3/5})\,r^{-3/5}_*\, \mathcal{B}^{-4/5} \mathcal{C}^{1/2} \mathcal{D}^{-4/5} \mathcal{Q}^{3/5}, \\
H &= [1 \times 10^3 \text{ cm}](\alpha^{-1/10} m^{9/10} \dot{m}^{1/5})\,r^{21/20}_*\,\mathcal{A} \mathcal{B}^{-6/5} \mathcal{C}^{1/2} \mathcal{D}^{-3/5} \mathcal{E}^{-1/2} \mathcal{Q}^{1/5}, \\
\rho_0 &= [4 \times 10^1 \text{ g~cm}^{-3}](\alpha^{-7/10} m^{-7/10} \dot{m}^{2/5})\,r^{-33/20}_*\,\mathcal{A}^{-1} \mathcal{B}^{3/5} \mathcal{D}^{-1/5} \mathcal{E}^{1/2} \mathcal{Q}^{2/5}, \\
T &= [7 \times 10^8 \text{ K}](\alpha^{-1/5} m^{-1/5} \dot{m}^{2/5})\,r^{-9/10}_*\,\mathcal{B}^{-2/5} \mathcal{D}^{-1/5}\mathcal{Q}^{2/5}, \\
\beta/(1-\beta) &= [7 \times 10^{-3}](\alpha^{-1/10} m^{-1/10} \dot{m}^{-4/5})\,r^{21/20}_*\,\mathcal{A}^{-1} \mathcal{B}^{9/5} \mathcal{D}^{2/5} \mathcal{E}^{1/2} \mathcal{Q}^{-4/5}, \\
\tau_{ff}/{\tau}_{es} &= [2 \times 10^{-6}](\dot{m}^{-1})\,r^{3/2}_*\,\mathcal{A}^{-1} \mathcal{B}^{2} \mathcal{D}^{1/2}\mathcal{E}^{1/2} \mathcal{Q}^{-1},
\end{aligned}
F Σ H ρ 0 T β / ( 1 − β ) τ f f / τ es = [ 7 × 1 0 26 erg cm − 2 s − 1 ] ( m − 1 m ˙ ) r ∗ − 3 B − 1 C − 1/2 Q , = [ 9 × 1 0 4 g cm − 2 ] ( α − 4/5 m 1/5 m ˙ 3/5 ) r ∗ − 3/5 B − 4/5 C 1/2 D − 4/5 Q 3/5 , = [ 1 × 1 0 3 cm ] ( α − 1/10 m 9/10 m ˙ 1/5 ) r ∗ 21/20 A B − 6/5 C 1/2 D − 3/5 E − 1/2 Q 1/5 , = [ 4 × 1 0 1 g cm − 3 ] ( α − 7/10 m − 7/10 m ˙ 2/5 ) r ∗ − 33/20 A − 1 B 3/5 D − 1/5 E 1/2 Q 2/5 , = [ 7 × 1 0 8 K ] ( α − 1/5 m − 1/5 m ˙ 2/5 ) r ∗ − 9/10 B − 2/5 D − 1/5 Q 2/5 , = [ 7 × 1 0 − 3 ] ( α − 1/10 m − 1/10 m ˙ − 4/5 ) r ∗ 21/20 A − 1 B 9/5 D 2/5 E 1/2 Q − 4/5 , = [ 2 × 1 0 − 6 ] ( m ˙ − 1 ) r ∗ 3/2 A − 1 B 2 D 1/2 E 1/2 Q − 1 ,
Inner region: P = P rad P=P_\text{rad} P = P rad , κ = κ es \kappa=\kappa_\text{es} κ = κ es F = [ 7 × 10 26 erg cm − 2 s − 1 ] ( m − 1 m ˙ ) r ∗ − 3 B − 1 C − 1 / 2 Q , Σ = [ 5 g cm − 2 ] ( α − 1 m ˙ − 1 ) r ∗ 3 / 2 A − 2 B 3 C 1 / 2 E Q − 1 , H = [ 1 × 10 5 cm ] ( m ˙ ) A 2 B − 3 C 1 / 2 D − 1 E − 1 Q , ρ 0 = [ 2 × 10 − 5 g cm − 3 ] ( α − 1 m − 1 m ˙ − 2 ) r ∗ 3 / 2 A − 4 B 6 D E 2 Q − 2 , T = [ 5 × 10 7 K ] ( α − 1 / 4 m − 1 / 4 ) r ∗ − 3 / 8 A − 1 / 2 B 1 / 2 E 1 / 4 , β / ( 1 − β ) = [ 4 × 10 − 6 ] ( α − 1 / 4 m − 1 / 4 m ˙ − 2 ) r ∗ 21 / 8 A − 5 / 2 B 9 / 2 D E 5 / 4 Q − 2 , ( τ f f τ e s ) 1 / 2 = [ 1 × 10 − 4 ] ( α − 17 / 16 m − 1 / 16 m ˙ − 2 ) r ∗ 93 / 32 A − 25 / 8 B 41 / 8 C 1 / 2 D 1 / 2 E 25 / 16 Q − 2 . \begin{aligned}
F &= [7 \times 10^{26} \text{ erg~cm}^{-2}~\text{s}^{-1}](m^{-1} \dot{m})\,r^{-3}_*\, \mathcal{B}^{-1} \mathcal{C}^{-1/2} \mathcal{Q}, \\
\Sigma &= [5 \text{ g~cm}^{-2}](\alpha^{-1} \dot{m}^{-1})\,r^{3/2}_*\, \mathcal{A}^{-2}\mathcal{B}^{3} \mathcal{C}^{1/2}\mathcal{E} \mathcal{Q}^{-1}, \\
H &= [1 \times 10^5 \text{ cm}](\dot{m})\,\mathcal{A}^2 \mathcal{B}^{-3} \mathcal{C}^{1/2} \mathcal{D}^{-1} \mathcal{E}^{-1} \mathcal{Q}, \\
\rho_0 &= [2 \times 10^{-5} \text{ g~cm}^{-3}](\alpha^{-1} m^{-1} \dot{m}^{-2})\,r^{3/2}_*\,\mathcal{A}^{-4} \mathcal{B}^{6} \mathcal{D} \mathcal{E}^{2} \mathcal{Q}^{-2}, \\
T &= [5 \times 10^7 \text{ K}](\alpha^{-1/4} m^{-1/4})\,r^{-3/8}_*\,\mathcal{A}^{-1/2}\mathcal{B}^{1/2} \mathcal{E}^{1/4}, \\
\beta/(1-\beta) &= [4 \times 10^{-6}](\alpha^{-1/4} m^{-1/4} \dot{m}^{-2})\,r^{21/8}_*\,\mathcal{A}^{-5/2} \mathcal{B}^{9/2} \mathcal{D} \mathcal{E}^{5/4} \mathcal{Q}^{-2}, \\
(\tau_{ff}\tau_{es})^{1/2} &= [1 \times 10^{-4}](\alpha^{-17/16} m^{-1/16} \dot{m}^{-2})\,r^{93/32}_*\,\mathcal{A}^{-25/8} \mathcal{B}^{41/8}\mathcal{C}^{1/2} \mathcal{D}^{1/2}\mathcal{E}^{25/16} \mathcal{Q}^{-2}.
\end{aligned}
F Σ H ρ 0 T β / ( 1 − β ) ( τ f f τ es ) 1/2 = [ 7 × 1 0 26 erg cm − 2 s − 1 ] ( m − 1 m ˙ ) r ∗ − 3 B − 1 C − 1/2 Q , = [ 5 g cm − 2 ] ( α − 1 m ˙ − 1 ) r ∗ 3/2 A − 2 B 3 C 1/2 E Q − 1 , = [ 1 × 1 0 5 cm ] ( m ˙ ) A 2 B − 3 C 1/2 D − 1 E − 1 Q , = [ 2 × 1 0 − 5 g cm − 3 ] ( α − 1 m − 1 m ˙ − 2 ) r ∗ 3/2 A − 4 B 6 D E 2 Q − 2 , = [ 5 × 1 0 7 K ] ( α − 1/4 m − 1/4 ) r ∗ − 3/8 A − 1/2 B 1/2 E 1/4 , = [ 4 × 1 0 − 6 ] ( α − 1/4 m − 1/4 m ˙ − 2 ) r ∗ 21/8 A − 5/2 B 9/2 D E 5/4 Q − 2 , = [ 1 × 1 0 − 4 ] ( α − 17/16 m − 1/16 m ˙ − 2 ) r ∗ 93/32 A − 25/8 B 41/8 C 1/2 D 1/2 E 25/16 Q − 2 .
The radial functions A , . . . , Q \mathcal{A},...,\mathcal{Q} A , ... , Q are defined in terms of y = r / M y=\sqrt{r/M} y = r / M and a ∗ = a / M a_*=a/M a ∗ = a / M as:
A = 1 + a ∗ 2 y − 4 + 2 a ∗ 2 y − 6 , B = 1 + a ∗ y − 3 , C = 1 − 3 y − 2 + 2 a ∗ y − 3 , D = 1 − 2 y − 2 + a ∗ 2 y − 4 , E = 1 + 4 a ∗ 2 y − 4 − 4 a ∗ 2 y − 6 + 3 a ∗ 4 y − 8 , Q 0 = 1 + a ∗ y − 3 y ( 1 − 3 y − 2 + 2 a ∗ y − 3 ) 1 / 2 , \begin{aligned}
\mathcal{A}&=1+a_*^2y^{-4}+2a_*^2y^{-6}, \\
\mathcal{B}&=1+a_*y^{-3}, \\
\mathcal{C}&=1-3y^{-2}+2a_*y^{-3}, \\
\mathcal{D}&=1-2y^{-2}+a_*^2y^{-4}, \\
\mathcal{E}&=1+4a_*^2y^{-4}-4a_*^2y^{-6}+3a_*^4y^{-8}, \\
\mathcal{Q}_0&=\frac{1+a_*y^{-3}}{y(1-3y^{-2}+2a_*y^{-3})^{1/2}},
\end{aligned}
A B C D E Q 0 = 1 + a ∗ 2 y − 4 + 2 a ∗ 2 y − 6 , = 1 + a ∗ y − 3 , = 1 − 3 y − 2 + 2 a ∗ y − 3 , = 1 − 2 y − 2 + a ∗ 2 y − 4 , = 1 + 4 a ∗ 2 y − 4 − 4 a ∗ 2 y − 6 + 3 a ∗ 4 y − 8 , = y ( 1 − 3 y − 2 + 2 a ∗ y − 3 ) 1/2 1 + a ∗ y − 3 ,
Q = Q 0 [ y − y 0 − 3 2 a ∗ ln ( y y 0 ) − 3 ( y 1 − a ∗ ) 2 y 1 ( y 1 − y 2 ) ( y 1 − y 3 ) ln ( y − y 1 y 0 − y 1 ) ] − Q 0 [ 3 ( y 2 − a ∗ ) 2 y 2 ( y 2 − y 1 ) ( y 2 − y 3 ) ln ( y − y 2 y 0 − y 2 ) − 3 ( y 3 − a ∗ ) 2 y 3 ( y 3 − y 1 ) ( y 3 − y 2 ) ln ( y − y 3 y 0 − y 3 ) ] . \begin{aligned}
\mathcal{Q}&=\mathcal{Q}_0\left[y-y_0-\frac{3}{2}a_*\ln\left(\frac{y}{y_0}\right)-\frac{3(y_1-a_*)^2}{y_1(y_1-y_2)(y_1-y_3)}\ln\left(\frac{y-y_1}{y_0-y_1}\right)\right] \\
&-\mathcal{Q}_0\left[\frac{3(y_2-a_*)^2}{y_2(y_2-y_1)(y_2-y_3)}\ln\left(\frac{y-y_2}{y_0-y_2}\right)-\frac{3(y_3-a_*)^2}{y_3(y_3-y_1)(y_3-y_2)}\ln\left(\frac{y-y_3}{y_0-y_3}\right)\right].
\end{aligned}
Q = Q 0 [ y − y 0 − 2 3 a ∗ ln ( y 0 y ) − y 1 ( y 1 − y 2 ) ( y 1 − y 3 ) 3 ( y 1 − a ∗ ) 2 ln ( y 0 − y 1 y − y 1 ) ] − Q 0 [ y 2 ( y 2 − y 1 ) ( y 2 − y 3 ) 3 ( y 2 − a ∗ ) 2 ln ( y 0 − y 2 y − y 2 ) − y 3 ( y 3 − y 1 ) ( y 3 − y 2 ) 3 ( y 3 − a ∗ ) 2 ln ( y 0 − y 3 y − y 3 ) ] .
Here y 0 = r ms / M y_0=\sqrt{r_\text{ms}/M} y 0 = r ms / M , and y 1 , y 2 , y 3 y_1,y_2,y_3 y 1 , y 2 , y 3 are the three roots of y 3 − 3 y + 2 a ∗ = 0 y^3-3y+2a_*=0 y 3 − 3 y + 2 a ∗ = 0 ; that is
y 1 = 2 cos [ ( cos − 1 a ∗ − π ) / 3 ] , y 2 = 2 cos [ ( cos − 1 a ∗ + π ) / 3 ] , y 3 = − 2 cos [ ( cos − 1 a ∗ ) / 3 ] . \begin{aligned}
y_1&=2\cos[(\cos^{-1}a_*-\pi)/3], \\
y_2&=2\cos[(\cos^{-1}a_*+\pi)/3], \\
y_3&=-2\cos[(\cos^{-1}a_*)/3].
\end{aligned}
y 1 y 2 y 3 = 2 cos [( cos − 1 a ∗ − π ) /3 ] , = 2 cos [( cos − 1 a ∗ + π ) /3 ] , = − 2 cos [( cos − 1 a ∗ ) /3 ] .
Slim Disks
In the thin disks, the accretion is radiatively efficient.
As the accretion rate is large, the radial velocity is large and the disk is thick enough, to trigger another cooling mechanism: advection.
Without the assumptions of radiative efficiency and Keplerian angular momentum, it is no longer possible to find an analytic solution to the system of equations.
ADAFs
The ADAF, or advection-dominated accretion flow, solution also involves cooling. It usually has low luminosity while the slim disk has high luminosity, because nearly all of the viscously dissipated energy is advected into the black hole rather than radiated.
Using scaling: r ∗ = r c 2 / G M r_*=rc^2/GM r ∗ = r c 2 / GM , m = M / M ⊙ m=M/M_\odot m = M / M ⊙ and m ˙ = M ˙ c 2 / L Edd \dot{m}=\dot{M}c^2/L_\text{Edd} m ˙ = M ˙ c 2 / L Edd .
v = [ − 3.00 × 10 10 cm s − 1 ] α c 1 r ∗ − 1 / 2 , Ω = [ 2.03 × 10 5 s − 1 ] c 2 m − 1 r ∗ − 3 / 2 , c S 2 = [ 9.00 × 10 20 cm s − 2 ] c 3 r ∗ − 1 , ρ = [ 1.07 × 10 − 5 g cm − 3 ] α − 1 c 1 − 1 c 3 − 1 / 2 m − 1 m ˙ r ∗ − 3 / 2 , P = [ 9.67 × 10 15 g cm − 1 s − 2 ] α − 1 c 1 − 1 c 3 1 / 2 m − 1 m ˙ r ∗ − 5 / 2 , B = [ 4.93 × 10 8 G ] α − 1 / 2 ( 1 − β m ) 1 / 2 c 1 − 1 / 2 c 3 1 / 4 m − 1 / 2 m ˙ 1 / 2 r ∗ − 5 / 4 , q + = [ 2.94 × 10 21 erg cm − 3 s − 1 ] ϵ ′ c 3 1 / 2 m − 2 m ˙ r ∗ − 4 , τ e s = [ 1.75 ] α − 1 c 1 − 1 m ˙ r ∗ − 1 / 2 , \begin{aligned}
v &= [-3.00 \times 10^{10} \text{ cm~s}^{-1}]\alpha c_1 r_*^{-1/2}, \\
\Omega &= [2.03 \times 10^5 \text{ s}^{-1}] c_2 m^{-1} r_*^{-3/2}, \\
c_S^2 &= [9.00 \times 10^{20} \text{ cm~s}^{-2}] c_3 r_*^{-1}, \\
\rho &= [1.07 \times 10^{-5} \text{ g~cm}^{-3}] \alpha^{-1} c_1^{-1} c_3^{-1/2} m^{-1} \dot{m} r_*^{-3/2}, \\
P &= [9.67 \times 10^{15} \text{ g~cm}^{-1}~\text{s}^{-2}] \alpha^{-1} c_1^{-1} c_3^{1/2} m^{-1} \dot{m} r_*^{-5/2}, \\
B &= [4.93 \times 10^8 \text{ G}] \alpha^{-1/2} (1-\beta_m)^{1/2} c_1^{-1/2} c_3^{1/4} m^{-1/2} \dot{m}^{1/2} r_*^{-5/4}, \\
q^+ &= [2.94 \times 10^{21} \text{ erg~cm}^{-3}~\text{s}^{-1}] \epsilon^\prime c_3^{1/2} m^{-2} \dot{m} r_*^{-4}, \\
\tau_\mathrm{es} &= [1.75] \alpha^{-1} c_1^{-1} \dot{m} r_*^{-1/2},
\end{aligned}
v Ω c S 2 ρ P B q + τ es = [ − 3.00 × 1 0 10 cm s − 1 ] α c 1 r ∗ − 1/2 , = [ 2.03 × 1 0 5 s − 1 ] c 2 m − 1 r ∗ − 3/2 , = [ 9.00 × 1 0 20 cm s − 2 ] c 3 r ∗ − 1 , = [ 1.07 × 1 0 − 5 g cm − 3 ] α − 1 c 1 − 1 c 3 − 1/2 m − 1 m ˙ r ∗ − 3/2 , = [ 9.67 × 1 0 15 g cm − 1 s − 2 ] α − 1 c 1 − 1 c 3 1/2 m − 1 m ˙ r ∗ − 5/2 , = [ 4.93 × 1 0 8 G ] α − 1/2 ( 1 − β m ) 1/2 c 1 − 1/2 c 3 1/4 m − 1/2 m ˙ 1/2 r ∗ − 5/4 , = [ 2.94 × 1 0 21 erg cm − 3 s − 1 ] ϵ ′ c 3 1/2 m − 2 m ˙ r ∗ − 4 , = [ 1.75 ] α − 1 c 1 − 1 m ˙ r ∗ − 1/2 ,
where v v v is the radial infall velocity and q + q^+ q + is the viscous dissipation of energy per unit volume.
The constants c 1 , c 2 , c 3 c_1,c_2,c_3 c 1 , c 2 , c 3 are given by
c 1 = ( 5 + 2 ε ′ ) 3 α 2 g ( α , ε ′ ) , c 2 = [ 2 ε ′ ( 5 + 2 ε ′ ) 9 α 2 g ( α , ε ′ ) ] 1 / 2 , c 3 = 2 ( 5 + 2 ε ′ ) 9 α 2 g ( α , ε ′ ) , \begin{aligned}
c_1&=\frac{(5+2\varepsilon')}{3\alpha^2}g(\alpha,\varepsilon'), \\
c_2&=\left[\frac{2\varepsilon'(5+2\varepsilon')}{9\alpha^2}g(\alpha,\varepsilon')\right]^{1/2}, \\
c_3&=\frac{2(5+2\varepsilon')}{9\alpha^2}g(\alpha,\varepsilon'),
\end{aligned}
c 1 c 2 c 3 = 3 α 2 ( 5 + 2 ε ′ ) g ( α , ε ′ ) , = [ 9 α 2 2 ε ′ ( 5 + 2 ε ′ ) g ( α , ε ′ ) ] 1/2 , = 9 α 2 2 ( 5 + 2 ε ′ ) g ( α , ε ′ ) ,
where
ε ′ = 1 f adv ( 5 / 3 − γ g γ g − 1 ) , g ( α , ε ′ ) ≡ [ 1 + 18 α 2 ( 5 + 2 ε ′ ) 2 ] 1 / 2 − 1 , \begin{aligned}
\varepsilon'&=\frac{1}{f_\text{adv}}\left(\frac{5/3-\gamma_g}{\gamma_g-1}\right), \\
g(\alpha,\varepsilon')&\equiv\left[1+\frac{18\alpha^2}{(5+2\varepsilon')^2}\right]^{1/2}-1,
\end{aligned}
ε ′ g ( α , ε ′ ) = f adv 1 ( γ g − 1 5/3 − γ g ) , ≡ [ 1 + ( 5 + 2 ε ′ ) 2 18 α 2 ] 1/2 − 1 ,
and the parameter f adv f_\text{adv} f adv represents the fraction of viscously dissipated energy which is advected. The remaining amount 1 − f adv 1-f_\text{adv} 1 − f adv is radiated locally.