Bibcode
de Jager, C.; Lobel, A.; Israelian, G.
Referencia bibliográfica
Astronomy and Astrophysics, v.325, p.714-724
Fecha de publicación:
9
1997
Revista
Número de citas
20
Número de citas referidas
16
Descripción
The hypergiant ρ Cas is known for its variable rate of mass loss,
with an average value of about 10^-5^Msun_/yr, and the
supersonic value for the line-of-sight component of the microturbulent
velocity, about 11km/s. Emission components in Hα suggest the
presence of a thermally excited outer atmospheric region. Since
hydrodynamical turbulence in a stellar atmosphere turns rapidly into a
field of shock waves, and shock waves are known to be able to initiate a
stellar wind and heat stellar atmospheric layers, we have tried to
predict the rate of mass loss, the microturbulent velocity component and
the observed Hα profile by assuming a stochastic field of shock
waves. To that end we adopted a Kolmogoroffian spectrum of shock waves,
characterized by only one parameter: the maximum Mach number in front of
the shocks: M_1,max_. Behind every shock a thin hot region originates.
Spectroscopically, the thermal motions in these sheetlike regions cannot
be distinguished from the stochastic hydrodynamic (shock wave) motion
component, and therefore these hot regions add to the line broadening
and will also contribute to the observed 'microturbulence'. We find that
it is indeed possible to explain the observed rate of mass loss (we
derived log˙(M)=~-5(Msun_/yr)), as well as the high value
for the quasi-microturbulence (we calculated =~12km/s). The hot sheets
behind the shocks appear to be responsible for the observed
'microturbulence'; this thermal contribution is much larger than that of
the hydrodynamic (shock) motions, which is only 0.4 to 0.5km/s. Non-LTE
calculations of the Hα line profile show that the shocks, in
association with the observed time-dependent variation of T_eff_ can
reproduce aspects of the variable emission in Hα. These three
aspects of this star, viz. the observed rate of mass loss, the observed
supersonic 'microturbulence', as well as the Hα line profile can
be simulated by one parameter only: viz. M_1,max_=1.06 to 1.08, a value
that characterizes a fairly weak shock-wave field.