Astron. Astrophys. 343, 325-332 (1999)
3. Potential for the Kerr field
Relativistic gravitational fields can be interpreted as consisting of
three parts: the Newtonian (also Coulomb or gravitoelectric)
component, the dragging (gravitomagnetic) component, and the
space-geometry component. The Newtonian component is generated by
mass-density and is given essentially by the gradient of the
component of the spacetime metric.
The dragging component is generated by mass-currents and determined by
curl of . The space-geometry
component (determined by ) has no
classical analog. This view and, in particular, the analogy with
electromagnetism are most straightforward within the linearized
approximation, but can be given a precise and invariant meaning even
in strong fields (Thorne et al. 1986; Jantzen et al. 1992, and
references cited therein). Let us compose the potential for the Kerr
spacetime in a way that acknowledges this approach.
3.1. The Newtonian component
Cutting the Kerr manifold at , one
can obtain the spacetime which is free of causality-violating regions.
The cut leads to jumps in derivatives of the metric at
which are interpreted as a thin
massive layer. This induced mass spreads over the
hypersurface and consists of the
attractive singular ring ( ,
) of infinite positive mass density,
spanned by the repulsive disc ( ,
) of negative mass density.
Constructing the causally maximal extension of the Kerr metric, Keres
(1967) and Israel (1970) showed that the Newtonian field generated by
the massive layer corresponds to the
potential 2
![[EQUATION]](img29.gif)
The structure of this field was shown in Semerák (1995; cf.
Fig. 2 there) by depicting its lines in the
( )-plane. We will use the
Keres-Israel potential as a scalar "seed" of our model. With
given by Eq. (10), Eqs. (6)-(8) read
![[EQUATION]](img32.gif)
Separated first integrals of these equations (analogy of Carter's
equations for the Kerr spacetime) were found by Israel (1970). It was
illustrated in Semerák (1996) that Eqs. (11)-(13) often yield
trajectories indiscernible from their exact-Kerr counterparts computed
from Eqs. (1)-(3). However, they do not contain the terms linear in
velocities which embody the very characteristic feature of the Kerr
geometry - the frame-dragging effects.
3.2. The dragging component
In this section, we are led by analogy with classical electrodynamics
and by observation that the Kerr dipole-like gravitomagnetic field
resembles the Kerr-Newman magnetic field. One thus arrives at the
potential which incorporates dragging in the form
![[EQUATION]](img33.gif)
where and the vector potential
is given by that of the Kerr-Newman
electromagnetic field, , with
Q (electric charge of the Kerr-Newman centre) replaced by
(the extra factor of 2 is ascribed
to the tensorial character of gravity and the minus sign to its
attractive nature) - i.e., . Similar
(just half) correction for the dragging was considered by Dadhich
(1985) for a special case of particles with zero axial angular
momentum. The added term really
introduces the desired dragging terms into the Eqs. (11)-(13): they
read now
![[EQUATION]](img40.gif)
Note that the contravariant 3-potential obtained by using the
inversion of the Kerr 3-metric, ,
is
![[EQUATION]](img42.gif)
where and
;
equals the shift vector of Thorne et al. (1986) which stands for the
potential of the gravitomagnetic field in this reference.
3.3. The space-geometry component
The space curvature cannot be understood directly within the Newtonian
or electromagnetic analogy. It may only be included by introducing ad
hoc corrections into the form (14):
![[EQUATION]](img46.gif)
This potential leads to equations of motion
![[EQUATION]](img47.gif)
The only point in which Eqs. (20) and (21) differ from the
relativistic Eqs. (1)-(2) is that the relativistic variable
- given by
(E and
stand for the particle's energy and
axial angular momentum at infinity) - is replaced by m in the
classical model. This distinction reflects, however, the conflict
between the very roots of classical physics (where time parameter is
universal) and relativity (where proper time and some coordinate time
occur, related to each other in a specific way at each point). Notice
that Eq. (22) differs from (3) also in several other points.
3.4. Specific features of motion in the pseudo-Kerr potential
Independence of the Lagrangian on
t and implies two constants
of motion,
![[EQUATION]](img53.gif)
where . The Kerr axial angular
momentum at infinity contains (again, as in Eqs. (20)-(21))
instead of m
( is the angular velocity with which
the field rotates relative to an observer standing at infinity). For
large r one obtains the usual forms of the energy and axial
angular momentum in the Newtonian central gravitational field:
![[EQUATION]](img56.gif)
Let us determine the acceleration
of an observer orbiting uniformly ( )
at ,
. We will define acceleration as a
specific force necessary to keep the observer in the orbit, i.e. as
the minus acceleration of a free particle having
at a given point. According to
Eqs. (20)-(22), we find
![[EQUATION]](img62.gif)
This 3-acceleration differs from the space part of 4-acceleration
of the Kerr stationary observer only by the absence of the
multiplicative factor (square of the
time-component of the observer's 4-velocity) [cf. Semerák 1993,
Eqs. (37)-(39)].
For a static observer ( ) one
obtains, in particular,
![[EQUATION]](img65.gif)
Hence, the field is repulsive at
in the sense that the radial component of (30) is negative there.
According to (27)-(29), the stationary observer needs no thrust
(i) at on the axis
( ), and (ii) in the equatorial
plane if his angular velocity is .
The latter agrees exactly with the Keplerian angular velocity of an
equatorial observer orbiting along a circular geodesic in the Kerr
spacetime.
Important circular geodesics in the equatorial plane, on the other
hand, are not reproduced properly by the potential (19), viz. the
equation for marginally stable orbits reads
![[EQUATION]](img70.gif)
and for marginally bound orbits
![[EQUATION]](img71.gif)
The correct equations have respectively the forms
![[EQUATION]](img72.gif)
and
![[EQUATION]](img73.gif)
In the Schwarzschild case, for instance, both our equations imply
.
In any pseudo-Newtonian description of a rotating black hole, the
main difficulty is to simulate the presence of the horizon and of the
dragging effects with an acceptable precision. Both these phenomena
are outside the scope of Newtonian physics. Our potential accounts for
the frame-dragging effects, and especially in the intermediate and
large distances provides a good fit, whereas it does not describe
correctly the innermost region where the horizon and important
circular orbits lie. In order to account for the horizon, one would
have to start from the scalar potential which diverges to
there. The Keres-Israel potential
(10), instead, reaches only at the
very singularity . The potential
proposed by Artemova et al. (1996) is a better alternative in this
respect, being the simplest generalization of the
Paczy ski-Wiita potential to
the Kerr case which reproduces the horizon and approximates the
important orbits. Also, the epicyclic frequency of small radial
oscillation , important in the theory
of discoseismology, is not reproduced with good accuracy by potentials
(10) and (19) although it does show a maximum, typical for a
relativistic . Apparently, trying to
incorporate different manifestations of the frame-dragging accurately,
one may end with a long expression without practical sense.
To summarize, each particular relativistic effect can be well
simulated within classical physics, but pseudo-Newtonian modelling of
the complete relativistic situation has only a restricted validity. In
order to clarify the value of our potential, we have carried out an
extensive computation of trajectories and introduced a criterion which
determines the accuracy of the pseudo-Newtonian model.
© European Southern Observatory (ESO) 1999
Online publication: March 1, 1999
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