Epicyclic frequency explained

In astrophysics, particularly the study of accretion disks, the epicyclic frequency is the frequency at which a radially displaced fluid parcel will oscillate. It can be referred to as a "Rayleigh discriminant". When considering an astrophysical disc with differential rotation

\Omega

, the epicyclic frequency

\kappa

is given by

\kappa2\equiv

2\Omega
R
d
dR

(R2\Omega)

, where R is the radial co-ordinate.[1]

This quantity can be used to examine the 'boundaries' of an accretion disc: when

\kappa2

becomes negative, then small perturbations to the (assumed circular) orbit of a fluid parcel will become unstable, and the disc will develop an 'edge' at that point. For example, around a Schwarzschild black hole, the innermost stable circular orbit (ISCO) occurs at three times the event horizon, at

6GM/c2

.

For a Keplerian disk,

\kappa=\Omega

.

Derivation

An astrophysical disk can be modeled as a fluid with negligible mass compared to the central object (e.g. a star) and with negligible pressure. We can suppose an axial symmetry such that

\Phi(r,z)=\Phi(r,-z)

. Starting from the equations of movement in cylindrical coordinates : \begin \ddot r - r \dot \theta^2 &= -\partial_r \Phi \\r \ddot \theta + 2 \dot r\dot\theta &= 0 \\ \ddot z &= -\partial_z \Phi \end

The second line implies that the specific angular momentum is conserved. We can then define an effective potential

\Phieff=\Phi-

1
2
2\theta
r

2=\Phi-

h2
2r2

and so : \begin\ddot r &= -\partial_r \Phi_\\ \ddot z &= - \partial_z \Phi_\end

We can apply a small perturbation

\delta\vecr=\deltar\vecer+\deltaz\vecez

to the circular orbit : \vec r = r_0 \vec e_r + \delta \vec r So, \ddot + \delta \ddot = -\vec \nabla \Phi_(\vec r + \delta \vec r)\approx-\vec \nabla \Phi_ (\vec r) - \partial_r^2 \Phi_(\vec r)\delta r - \partial_z^2 \Phi_(\vec r)\delta z

And thus : \begin \delta \ddot r &= - \partial_r^2 \Phi_ \delta r = -\Omega_r^2 \delta r\\\delta \ddot z &= - \partial_r^2 \Phi_ \delta z = -\Omega_z^2 \delta z\end We then note \kappa^2 = \Omega_r^2 = \partial_r^2\Phi_ = \partial_r^2\Phi + \fracIn a circular orbit

2=r
h
c

3\partialr\Phi

. Thus : \kappa^2 = \partial_r^2\Phi + \frac\partial_r \PhiThe frequency of a circular orbit is
2
\Omega
c

=

1r
\partial

r\Phi

which finally yields :\kappa^2=4\Omega_c^2 + 2r\Omega_c \frac

References

  1. p161, Astrophysical Flows, Pringle and King 2007