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Astron. Astrophys. 353, 641-645 (2000)
3. Methodology and the core envelope model
For spherically symmetric and static configurations we make use of
the metric
![[EQUATION]](img52.gif)
where and
are functions of r alone. The
Oppenheimer-Volkoff (O-V) equations, resulting from Einstein's field
equations, for systems with isotropic pressure P and
energy-density E can be written as
![[EQUATION]](img55.gif)
where is the mass, contained
within the radius r, and the prime denotes radial
derivative.
The core-envelope model consists of a core with most stiff EOS in
the region and an envelope with a
polytropic EOS in the region as
given below
(i) The core:
For the models of neutron stars considered here, we have chosen the
core of most stiff material (Eq. (1)) as
![[EQUATION]](img59.gif)
where is the value of density at
the surface of the configuration, where pressure vanishes.
(ii) The envelope:
The envelope of this model is given by the equation of state
![[EQUATION]](img60.gif)
or
![[EQUATION]](img61.gif)
where K is a constant to be worked out by the matching of
various variables at the core-envelope boundary.
At the boundary, , the continuity
of , and
require
![[EQUATION]](img65.gif)
where is given by (see, e.g.,
Tooper 1965)
![[EQUATION]](img66.gif)
Thus, the continuity of , at the
boundary gives
![[EQUATION]](img67.gif)
Thus, the continuity of and
at the core-envelope boundary is
ensured, for the static and spherically symmetric configuration.
The coupled Eqs. (3), (4), (5), are solved along with Eqs. (1) and
(6) for the boundary conditions (7) and (8) [at the core-envelope
boundary, ], and the boundary
conditions, ,
,
at the external boundary, .
For the sake of numerical simplification, we assign the central
density, . It is seen that the degree
of softness of the envelope is restricted by the inequality,
. For the minimum value of
, we obtain various quantities, such
as, core mass, , core radius,
, density at the core-envelope
boundary, , total mass, M, and
the corresponding radius, R, of the configuration in
dimensionless form as shown in Table 1 for various assigned
values of the central pressure to density ratio,
.
![[TABLE]](img108.gif)
Table 1. Properties of the causal core-envelope models, with a core given by the most stiff EOS, , and the envelope is characterized by the polytropic EOS, (d d , such that, all the parameters, and the speed of sound, , are continuous at the core-envelope boundary, . The maximum value of for the structure is obtained (Fig. 1), when the minimum value of the ratio of pressure to density at the core-envelope boundary, , reaches about 0.014. The maximum value of the binding-energy per baryon, where is the rest mass of the configuration] also occurs for the maximum stable value of u. The subscript `0' and `b' represent, the values of respective quantities at the centre, and at the core-envelope boundary. stands for the surface redshift. The calculations are performed for an assigned value of the central energy-density, . The slanted values represent the limiting case upto which the structure remains dynamically stable. Dimensionless values of various quantities for 0.014
To determine the stability of the models given in Table 1, we
need to draw the mass-radius diagram for the structures. For this
purpose, we have normalized the boundary density,
g cm-3, and obtained the
mass-radius diagram as shown in Fig. 1 [Notice that the value of
chosen in this way (and hence also
the mass and the radius obtained in conventional units as shown in
Fig. 1) is purely arbitrary. These values have nothing to do with the
actual maximum mass and the corresponding radius of the stable neutron
star obtained in the present paper. The choice of
does not affect the maximum value of
u upto which the structure remains dynamically stable]. The
maximum stable value of u of the whole configuration is
obtained as 0.3574, which would determine the maximum mass of the
stable neutron star from the knowledge of the rotation period of PSR
1937 + 214, or PSR 1957 + 20. It is interesting to note that for this
value of u, the binding energy per baryon,
, where
is the rest-mass (Zeldovich &
Novikov 1978) of the configuration] also approaches maximum
( ) as shown in Table 1.
![[FIGURE]](img125.gif) |
Fig. 1. Mass-Radius diagram of the model for an assigned value of g cm-3 at the core-envelope boundary , such that the ratio of pressure to density at reaches about 0.014. The pressure, energy-density, , and the speed of sound, are continuous at the core-envelope boundary.
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Koranda et al.(1997) have obtained the following empirical formula
for the class of minimum period EOSs which is fairly insensitive to
the matching density
![[EQUATION]](img127.gif)
where is the (minimum) rotation
period of the maximal (uniformly) rotating configuration, and M
and R are maximum mass and the corresponding size of the
non-rotating configuration. Rewriting Eq. (9) in terms of compaction
parameter, , and angular velocity
we obtain
![[EQUATION]](img131.gif)
where is the maximum value of
u of the non-rotating configuration, such that the
configuration becomes dynamically unstable when u exceeds
, and R represents the
corresponding radius of the configuration.
Let us denote the average density of the configuration by
[because
, or
] by using Eq. (10) we obtain
![[EQUATION]](img136.gif)
and,
![[EQUATION]](img137.gif)
Thus, the average density of the configuration depends only upon
the rotation period, and not upon the compaction parameter u.
Therefore, it is clear from Eqs. (11) - (12) that for a given value of
the rotation period, , the maximum
mass of the stable configuration depends only upon the maximum value
of u. For ms, Eq. (11) gives
the average density, , of the
configuration as g cm-3,
the substitution of in Eq. (12)
gives the maximum mass of the configuration,
and the corresponding radius,
km.
The ratio, M(envelope)/M(star), is about
, which may be relevant to explain
rotational irregularities in pulsars known as timing noise and
glitches (see, e.g., D' Allessandro 1997, and references therein).
© European Southern Observatory (ESO) 2000
Online publication: December 17, 1999
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