Astron. Astrophys. 341, 560-566 (1999)
3. Radiation forces
3.1. Flux around the star
Assuming that the potential of the outer parts of a rotating star
may be represented using the Roche approximation, the radius of
equipotential surfaces r is dependent on the angle to the pole
, and is found by the solution of
![[EQUATION]](img32.gif)
where is the angular velocity,
is the radius in the polar
direction, and M is the mass contained within the equipotential
surface. This has been solved for
geometrically by Collins & Harrington (1966). Deep within the star
the Roche approximation will be incorrect, although for the present
discussion, it is adequate. Indeed the region in which it is possible
to generate latitudinal metallic abundance anisotropies is found, a
posteriori , to be the outer parts of the envelope and so
, and Eq. 5 will be a good
representation.
The flux of the star f is proportional to the local gravity
(von Zeipel 1924):
![[EQUATION]](img37.gif)
Along the surface of any equipotential the local flux f is
higher at the pole than the equator (gravity darkening). This
difference between pole and equator is the root cause of the
latitudinal variation of the metallic abundance. It is noted that this
gravity darkening actually causes the meridional circulation, else
energy would not be conserved in the star. However, the change in flux
is not destroyed by the motions.
3.2. Radiation force on a trace element
The force on ions due to radiation
is dependent on the gradient of the
flux passing through that point, i.e.
. To facilitate the calculation of
the force along an equipotential the ratio of the forces in the radial
and latitudinal directions is now calculated. In the outer parts of
the star, the luminosity is a constant, and hence the flux varies with
distance r from the centre of the star as
. As the radiative force is
proportional to , then the ratio of
the latitudinal to radial components is
![[EQUATION]](img42.gif)
where s is the distance along an equipotential. Again, note
this is only an approximation as the unit vectors
and
are not orthogonal. This ratio is
shown in Fig. 1 for different rotation rates. As can be seen it is
typically , and therefore, perhaps
surprisingly, the radiative force around an equipotential is typically
similar to the radial radiative acceleration.
![[FIGURE]](img46.gif) |
Fig. 1. Ratio of latitudinal to radial radiative force defined from Eq. 4. The lines correspond to a rotation of 0.3, 0.4, 0.5, 0.6, 0.7, 0.8 and 0.9 of break-up velocity, where the uppermost line corresponds to the highest rotation, decreasing downwards.
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Michaud et al. (1976) see also Alecian & Artru (1990) have
discussed the radiative force due to lines on heavy elements. Their
expressions, along with Eq. 7, lead to the latitudinal force on on a
trace element (with a negligible gradient in the concentration of the
ions) of
![[EQUATION]](img48.gif)
where and
are the temperature and effective
temperature in units of K
respectively, r is the radius and
is the stellar radius. The atomic
parameters are enveloped in , and
is the atomic mass of the element
i.
With the inclusion of a non-zero concentration of ions the driving
lines become saturated, and the line force is reduced from Eq. 8:
![[EQUATION]](img55.gif)
(Alecian 1985). The reference concentration
is
![[EQUATION]](img57.gif)
where is the Rosseland mean
opacity, is the number density of
electrons and is an atomic parameter
containing line broadening effects.
© European Southern Observatory (ESO) 1999
Online publication: December 4, 1998
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