Density of a patch of an accretion disk

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SUMMARY

The discussion focuses on the density of a patch of an accretion disk, analyzing the balance of forces in hydrostatic equilibrium. The gravitational potential is expressed as ##\phi = -GM(R^2 + z^2)^{-1/2}##, leading to the density equation ##\rho = \rho_0 \mathrm{exp}[-\Omega^2 z^2 /(2c_s^2)]##. The ideal gas law is also addressed, with the relationship ##P = \frac{c_s^2}{\gamma} \rho## established for an adiabatic gas. The conversation emphasizes the importance of the adiabatic index ##\gamma## and the assumption of an isothermal static atmosphere.

PREREQUISITES
  • Understanding of hydrostatic equilibrium principles
  • Familiarity with the ideal gas law and its applications
  • Knowledge of gravitational potential in astrophysical contexts
  • Basic concepts of sound speed in gases, particularly adiabatic processes
NEXT STEPS
  • Study the derivation of gravitational potential in astrophysical disks
  • Learn about the implications of the adiabatic index ##\gamma## in different gas conditions
  • Explore the relationship between sound speed and pressure in isothermal atmospheres
  • Investigate the dynamics of accretion disks and their stability under various forces
USEFUL FOR

Astronomers, astrophysicists, and students studying fluid dynamics in astrophysical contexts will benefit from this discussion, particularly those focusing on accretion disk behavior and hydrostatic equilibrium principles.

ergospherical
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Homework Statement
A small patch of a thin accretion disk (around a point mass) at a radius where the angular velocity is ##\Omega## can be assumed to have an isothermal static atmosphere. Show that the density varies with ##z## (distance from the mid-plane) as\begin{align*}
\rho = \rho_0 \mathrm{exp}[-\gamma \Omega^2 z^2/(2c_s^2)]
\end{align*}(##\gamma## is adiabatic index)
Relevant Equations
Fluid equations
In the frame of the patch ##-(1/\rho) \nabla p = - \nabla \phi##, and putting ##\nabla p = (\partial p/\partial \rho) \nabla \rho = c_s^2 \nabla \rho## and taking the ##z## component gives\begin{align*}
-\frac{c_s^2}{\rho} \frac{\partial \rho}{\partial z} = -c_s^2 \frac{\partial(\log{\rho})}{\partial z} = \frac{\partial \phi}{\partial z}
\end{align*}integrate:\begin{align*}
\rho = \rho_0 \mathrm{exp}[-\phi/c_s^2]
\end{align*}What is the form of the potential ##\phi##? I thought ##\phi = \phi_{\mathrm{rot}} + \phi_{\mathrm{grav}} = -\frac{1}{2} \Omega^2 r^2 + \phi_{\mathrm{grav}}##, but the centrifugal potential has no ##z## dependence and I don't see why the gravitational potential ##\phi_{\mathrm{grav}}## should depend on ##\Omega##.
 
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Isn't the gravitation ##\Omega## dependent by the assumption of a "static atmosphere"?
 
use basic principles of hydrostatic equilibrium and consider the ideal gas law.
 
For an element ##m## of the accretion disk located on the central plane (z = 0), the gravitational attraction ##F_G## toward the central mass ##M## is balanced by the centrifugal force ##F_C## in the frame of ##m##. However, for ##z \neq 0##, the two forces no longer balance because of the tilt of ##F_G##. For small ##z##, the two forces produce a net downward force on ##m##. Thus, equilibrium in the z-direction requires an additional upward force (caused by pressure variation in the z-direction).

1683487906907.png
 
Cheers! The gravitational potential at the point labelled in the diagram is ##\phi = -GM(R^2 + z^2)^{-1/2}##, where ##R## is the cylindrical radial coordinate. Expanding to first order gives \begin{align*}
\phi = -\frac{GM}{R} + \frac{GM z^2}{2R^3} \implies \frac{\partial \phi}{\partial z} = -\frac{GMz}{R^3}
\end{align*}The circular speed of the disk ##v_C(R) = \sqrt{GM/R} = \Omega R## implies ##\Omega^2 = GM/R^3##, so equivalently ##\partial \phi / \partial z = -\Omega^2 z##. The momentum equation in the ##z## direction gives\begin{align*}
-c_s^2 \frac{\partial \log{\rho}}{\partial z} = \Omega^2 z \implies \rho = \rho_0 \mathrm{exp}[-\Omega^2 z^2 /(2c_s^2)]
\end{align*}Looks like I'm missing the adiabatic index ##\gamma##?
 
ergospherical said:
Looks like I'm missing the adiabatic index ##\gamma##?
Show that the ideal gas law can be written as ##P = \large \frac{c_s^2}{\gamma} \rho##.
 
For an adiabatic gas I have ##c_s^2 = (\partial p/\partial \rho) |_S##, and given the equation of state in the form ##p = K\rho^{\gamma}## that means ##c_s^2 = \gamma p / \rho##. But starting from the hydrostatic equation\begin{align*}
\frac{1}{\rho} \frac{\partial p}{\partial z} = \frac{\partial \phi}{\partial z}
\end{align*}it looks like I can exchange\begin{align*}
\frac{\partial p}{\partial z} = \frac{\partial p}{\partial \rho} \frac{\partial \rho}{\partial z} = c_s^2 \frac{\partial \rho}{\partial z}
\end{align*}
 
ergospherical said:
For an adiabatic gas I have ##c_s^2 = (\partial p/\partial \rho) |_S##, and given the equation of state in the form ##p = K\rho^{\gamma}## that means ##c_s^2 = \gamma p / \rho##.
Ok. Sound vibrations are assume to be adiabatic. Thus, we use ##(\partial p / \partial \rho) |_S## when calculating ##c_s^2##.

ergospherical said:
it looks like I can exchange\begin{align*}
\frac{\partial p}{\partial z} = \frac{\partial p}{\partial \rho} \frac{\partial \rho}{\partial z} = c_s^2 \frac{\partial \rho}{\partial z}
\end{align*}
The problem statement says to assume an isothermal static atmosphere. So, when considering how ##P## and ##\rho## vary with ##z##, we would assume ##T## remains constant. So, $$\frac{\partial p}{\partial z} = \left(\frac{\partial p}{\partial \rho}\right)_T \frac{\partial \rho}{\partial z} $$
 
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I've just noticed, the problem statement says that the adiabatic sound speed is ##c_s^2##, i.e. ##c_s^2 = \gamma p / \rho##, but the atmosphere is assumed isothermal - so ##c_s^2|_{\mathrm{iso}} = p / \rho = c_s^2 / \gamma##, which clears it up. Thanks!
 
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