Chandrasekhar virial equations explained

In astrophysics, the Chandrasekhar virial equations are a hierarchy of moment equations of the Euler equations, developed by the Indian American astrophysicist Subrahmanyan Chandrasekhar, and the physicist Enrico Fermi and Norman R. Lebovitz.[1] [2] [3]

Mathematical description

Consider a fluid mass

M

of volume

V

with density

\rho(x,t)

and an isotropic pressure

p(x,t)

with vanishing pressure at the bounding surfaces. Here,

x

refers to a frame of reference attached to the center of mass. Before describing the virial equations, let's define some moments.

The density moments are defined as

M=\intV\rhodx,Ii=\intV\rhoxidx,Iij=\intV\rhoxixjdx,Iijk=\intV\rhoxixjxkdx,Iijk\ell=\intV\rhoxixjxkx\elldx,etc.

the pressure moments are

\Pi=\intVpdx,\Pii=\intVpxidx,\Piij=\intVpxixjdx,\Piijk=\intVpxixjxkdxetc.

the kinetic energy moments are

Tij=

1
2

\intV\rhouiujdx,Tij;k=

1
2

\intV\rhouiujxkdx,Tij;k\ell=

1
2

\intV\rhouiujxkx\elldx,etc.

and the Chandrasekhar potential energy tensor moments are

Wij=-

1
2

\intV\rho\Phiijdx,Wij;k=-

1
2

\intV\rho\Phiijxkdx,Wij;k\ell=-

1
2

\intV\rho\Phiijxkx\elldx,etc.where\Phiij=G\intV\rho(x')

(xi-xi')(xj-xj')
|x-x'|3

dx'

where

G

is the gravitational constant.

All the tensors are symmetric by definition. The moment of inertia

I

, kinetic energy

T

and the potential energy

W

are just traces of the following tensors

I=Iii=\intV\rho|x|2dx,T=Tii=

1
2

\intV\rho|u|2dx,W=Wii=-

1
2

\intV\rho\Phidxwhere\Phi=\Phiii=\intV

\rho(x')
|x-x'|

dx'

Chandrasekhar assumed that the fluid mass is subjected to pressure force and its own gravitational force, then the Euler equations is

\rho

dui
dt

=-

\partialp
\partialxi

+\rho

\partial\Phi
\partialxi

,where

d
dt

=

\partial
\partialt

+uj

\partial
\partialxj

First order virial equation

2I
d
i
dt2

=0

Second order virial equation

1
2
2I
d
ij
dt2

=2Tij+Wij+\deltaij\Pi

In steady state, the equation becomes

2Tij+Wij=-\deltaij\Pi

Third order virial equation

1
6
d2Iijk
dt2

=2(Tij;k+Tjk;i+Tki;j)+Wij;k+Wjk;i+Wki;j+\deltaij\Pik+\deltajk\Pii+\deltaki\Pij

In steady state, the equation becomes

2(Tij;k+Tik;j)+Wij;k+Wik;j=-\deltaij\PiK-\deltaik\Pij

Virial equations in rotating frame of reference

The Euler equations in a rotating frame of reference, rotating with an angular velocity

\Omega

is given by

\rho

dui
dt

=-

\partialp
\partialxi

+\rho

\partial\Phi
\partialxi

+

1
2

\rho

\partial
\partialxi

|\Omega x x|2+2\rho\varepsiloni\ellu\ell\Omegam

where

\varepsiloni\ell

is the Levi-Civita symbol,
1
2

|\Omega x x|2

is the centrifugal acceleration and

2u x \Omega

is the Coriolis acceleration.

Steady state second order virial equation

In steady state, the second order virial equation becomes

2Tij+Wij+\Omega2Iij-\Omegai\OmegakIkj+2\epsiloni\ell\Omegam\intV\rhou\ellxjdx=-\deltaij\Pi

If the axis of rotation is chosen in

x3

direction, the equation becomes

Wij+\Omega2(Iij-\deltai3I3j)=-\deltaij\Pi

and Chandrasekhar shows that in this case, the tensors can take only the following form

Wij=\begin{pmatrix} W11&W12&0\\ W21&W22&0\\ 0&0&W33\end{pmatrix},Iij=\begin{pmatrix} I11&I12&0\\ I21&I22&0\\ 0&0&I33\end{pmatrix}

Steady state third order virial equation

In steady state, the third order virial equation becomes

2(Tij;k+Tik;j)+Wij;k+Wik;j+\Omega2Iijk-\Omegai\Omega\ellI\ell+2\varepsiloni\ell\Omegam\intV\rhou\ellxjxkdx=-\deltaij\Pik-\deltaik\Pij

If the axis of rotation is chosen in

x3

direction, the equation becomes

Wij;k+Wik;j+\Omega2(Iijk-\deltai3I3jk)=-(\deltaij\Pik+\deltaik\Pij)

Steady state fourth order virial equation

With

x3

being the axis of rotation, the steady state fourth order virial equation is also derived by Chandrasekhar in 1968.[4] The equation reads as
1
3

(2Wij;kl+2Wik;lj+2Wil;jk+Wij;k;l+Wik;l;j+Wil;j;k)+\Omega2(Iijkl-\deltai3I3jkl)=-(\deltaij\Pikl+\deltaik\Pilj+\deltail\Pijk)

Virial equations with viscous stresses

Consider the Navier-Stokes equations instead of Euler equations,

\rho

dui
dt

=-

\partialp
\partialxi

+\rho

\partial\Phi
\partialxi

+

\partial\tauik
\partialxk

,where\tauik=\rho\nu\left(

\partialui+
\partialxk
\partialuk-
\partialxi
2
3
\partialul
\partialxl

\deltaik\right)

and we define the shear-energy tensor as

Sij=\intV\tauijdx.

With the condition that the normal component of the total stress on the free surface must vanish, i.e.,

(-p\deltaik+\tauik)nk=0

, where

n

is the outward unit normal, the second order virial equation then be
1
2
2I
d
ij
dt2

=2Tij+Wij+\deltaij\Pi-Sij.

This can be easily extended to rotating frame of references.

See also

Notes and References

  1. Chandrasekhar, S; Lebovitz NR (1962). "The Potentials and the Superpotentials of Homogeneous Ellipsoids" (PDF). Ap. J. 136: 1037–1047. . . Retrieved March 24, 2012.
  2. Chandrasekhar, S; Fermi E (1953). "Problems of Gravitational Stability in the Presence of a Magnetic Field" (PDF). Ap. J. 118: 116. . . Retrieved March 24, 2012.
  3. Chandrasekhar, Subrahmanyan. Ellipsoidal figures of equilibrium. Vol. 9. New Haven: Yale University Press, 1969.
  4. Chandrasekhar, S. (1968). The virial equations of the fourth order. The Astrophysical Journal, 152, 293. http://repository.ias.ac.in/74364/1/93-p-OCR.pdf