 |  |
Astron. Astrophys. 357, 180-196 (2000)
3. Numerical simulations of the formation of detached, geometrically thin gas shells
In the following we present the results of a number of numerical
simulations that were carried out in an effort to investigate the
hydrodynamical details regarding the two competing scenarios currently
being discussed as possible explanations for the existence of thin
circumstellar CO shells. The goal is to find out whether both
scenarios are viable from a hydrodynamical point of view, and whether
we can find any clues as to what is the most likely explanation:
mass loss `eruption' , two-wind interaction , or a
combination of both .
3.1. Mass loss `eruption' models
Case A : the S Scuti scenario
In order to explain the observed IR spectral energy distribution of
the well-known carbon star S Sct, Groenewegen & de Jong
(1994) argued that a mass loss `eruption' must have taken place about
10 000 yrs ago. Based on their dust radiative transfer models they
conclude that the `eruption' lasted for about 1000 years at a rate of
. Their favored mass loss history is
indicated by the dashed line in Fig. 1.
![[FIGURE]](img41.gif) |
Fig. 1. Top: Two different mass loss `eruption' models investigated in this work: the mass loss history suggested by the properties of the CO shell of TT Cyg (Case B , solid), compared to the mass loss history proposed by Groenewegen & de Jong (1994) for S Sct (Case A , dashed). For the times labeled `1' to `10', the radial distribution of velocity and density is shown in Fig. 2. Middle: Gas velocity u (solid) and dust velocity w (dotted) as a function of time at a radial distance of cm, as obtained from two-component radiation hydrodynamics for the TT Cyg mass loss `eruption' model shown above. Bottom: Dust temperature as a function of time at radial distances of cm (upper) and cm (lower) for the TT Cyg mass loss `eruption' model, as obtained by DEXCEL from the condition of dust radiative equilibrium.
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Several remarks are in order. First, we point out that Groenewegen
& de Jong ignore the hydrodynamics of the problem. Instead, they
adopt a simple kinematic approach, assuming a uniform wind velocity of
16.5 km s-1, irrespective of the mass loss rate.
According to our radiation hydrodynamics calculations, this is
not a valid approximation (see below). Second, in order to
explain the dust emission at
100 µm, they have to
assume a rather high dust-to-gas ratio of
. We have recalculated their case
with our two-component radiation hydrodynamics code, adopting the same
stellar parameters, mass loss history, dust properties and dust-to-gas
ratio, and find that the resulting gas outflow velocity is as high as
80 km s-1 before the `eruption' (which is clearly
unrealistic) and about 10 km s-1 afterwards
(demonstrating that the outflow velocity is actually not
independent of the mass loss rate). Even though the radial dust
distribution is distinctly different in the kinematic and the
hydrodynamical case, both models contain the same total amount of dust
and perfectly fit the observed IR spectral energy distribution of
S Sct (not shown). Interestingly, the hydrodynamical model
calculations based on stellar evolution calculations with mass loss
can also explain the IR emission of S Sct (cf. Fig 18 of SSS98),
although the underlying mass loss history is completely different (top
panel of Fig. 7 below).
Finally, we have recalculated the case of Groenewegen & de Jong
with a more realistic dust-to-gas ratio of
, and find a gas outflow velocity of
19 km s-1 before the `eruption' (which is much more
reasonable) and of 6 km s-1 afterwards. This model
fails, however, to account for the dust emission observed at
100 µm.
In summary, we see no convincing arguments in favor of the mass
loss `eruption' scenario as far as the modeling of the dust
component is concerned.
Case B : the TT Cygni scenario
Even though no physical mechanism is presently known to produce
very short mass loss `eruptions' of the required strength (see however
recent claims by Schröder et al. 1998), it is nevertheless
tempting to relate the existence of the observed very thin CO shells
to this presumed phenomenon. According to Olofsson et al. 1998, the CO
shell of TT Cyg has a width of
cm and a radius of
cm. Assuming a constant
expansion velocity of 13 km s-1, this implies a mass
loss `eruption' that happened about 12 000 yrs ago and lasted for
about 500 yrs at a rate of
(estimated shell mass ). We have
constructed a schematic mass loss history in accordance with the above
mentioned data for TT Cyg (Fig. 1, solid line) and used it as a
boundary condition for a time-dependent hydrodynamical simulation of
the mass loss `eruption' scenario.
First we applied the DEXCEL code to this problem. The results are
displayed in the lower panels of Fig. 1 and in the left-hand column of
Fig. 2. Before the `eruption', the gas outflow velocity is
km s-1, well within
the observed range for carbon-rich AGB stars. The drift velocity of
the dust relative to the gas is considerable,
km s-1. During the
`eruption', the gas outflow velocity is slightly reduced due to
the increased optical depth of the heavy outflow,
km s-1, while the
drift velocity becomes essentially zero. After the `eruption', the
density of the wind is very low, so gas and dust decouple, as
indicated by the high drift velocity,
km s-1. At the same
time the gas velocity has declined to
km s-1, in agreement
with observational evidence for TT Cyg.
![[FIGURE]](img82.gif) |
Fig. 2a-d. Evolution of a shell of enhanced gas density produced by the TT Cyg mass loss `eruption' scenario defined in Fig. 1. Top to bottom: Radial distribution of a gas outflow velocity, b gas density, c differential shell mass (symbols mark the radial grid points; `measurements' of the half widths, , indicated by vertical and horizontal bars), and d relative shell width (dashed curve corresponding to const.). The labeled curves in the upper three panels correspond to times `1' to `10' indicated in Fig. 1. The left-hand column displays the results obtained with the DEXCEL two-component radiation hydrodynamics code (assuming , K, ), while the right-hand column shows the corresponding time sequence as obtained with the NEBEL one-component hydrodynamics code for the same , , at the inner boundary at cm. Different line styles serve to distinguish the curves and at different times.
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The gas shell produced by the mass loss `eruption' moves outward at
an average speed of
km s-1 (which in
this case practically coincides with the flow velocity at the center
of the shell, ), somewhat higher than
the Doppler velocity measured in the CO shell of TT Cyg. However,
the substantial velocity gradient across the shell that develops after
some time leads to a considerable broadening of the density structure
as it recedes from the star, and to a corresponding decline of its
amplitude (shell mass const.).
Beyond cm, the relative
thickness of the shell remains approximately constant at a value of
.
We have recalculated this test case with the NEBEL code, using the
DEXCEL results at cm (partly
shown in the lower panels of Fig. 1) as a time-dependent inner
boundary condition. The evolution of the ejected shell is shown in the
right-hand column of Fig. 2, while Fig. 3 displays details of the
structure as it appears 5 867.5 yrs after the end of the
`eruption'.
![[FIGURE]](img92.gif) |
Fig. 3. Radial distribution of gas velocity (top), particle number density (middle) as well as gas temperature and pressure (bottom, solid / dashed) at time yrs (between points 8 and 9), as obtained with the NEBEL one-component hydrodynamics code for the TT Cyg mass loss `eruption' scenario defined in Fig. 1. By this time the velocity plateau in the central part of the density peak has disappeared. Symbols (+) indicate the numerical grid.
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The propagation velocity of the gas shell produced by the mass loss
event is only marginally smaller than that found with DEXCEL,
km s-1. However, the
extended velocity plateau in the central part of the density peak
survives much longer than indicated by the DEXCEL results. As long as
it exists, the absolute shell width (FWHM) remains
approximately constant: cm,
corresponding to the original width of the `eruption',
. When the shell has moved out beyond
cm, the velocity plateau has
finally dissolved due to the presence of thermal pressure gradients.
The resulting positive mean velocity gradient then leads to some
noticeable broadening, such that the relative thickness of the
shell remains approximately constant at
.
In another NEBEL run, we have repeated this test problem without
any source terms in the energy equation. In this case, the temperature
drops far below the dust radiative equilibrium temperature due to
adiabatic cooling of the expanding outflow. As a consequence of the
concomitant overall reduction of the gas pressure, the average outflow
velocities are slightly reduced, and
km s-1. The velocity
plateau proves to be very stable in this situation, and the
absolute shell width remains essentially constant at
cm. This result demonstrates
that the broadening found in the above case where
is indeed caused by the thermal
pressure and not by numerical diffusion.
Clearly, the initial velocity plateau is the the result of the
constant outflow velocity during the mass ejection,
km s-1. The plateau
is eroded by rarefaction waves running into the density peak from the
edges. Hence, the life time of the velocity plateau is
, where
is the local sound speed. For the
non-adiabatic case,
km s-1, and
yrs, in close agreement wit the
NEBEL result. This estimate also explains the NEBEL results for the
adiabatic case, where is at least a
factor of 3 smaller.
We have to conclude that the strong dispersion of the density
structure as found with DEXCEL is an artifact, caused by substantial
numerical diffusion. The results obtained with NEBEL are much more
reliable, as expected for a second-order Godunov-type scheme. Still,
DEXCEL is needed to compute the wind acceleration in the inner region
of the dusty envelope.
Case C : modified TT Cygni scenario
For the sake of completeness, we have investigated a related mass
loss `eruption' model, which is obtained by reversing the mass loss
rates before and after the `eruption' in the TT Cyg scenario
studied before. In this case, called the modified TT Cyg
scenario in the following, we have a slow wind before, and a faster
wind after the mass loss event (upper panel of Fig. 4). There is no
known observational counterpart for this situation as far as AGB stars
are concerned, but it may be realized in other astrophysical
environments. Anyway, it is interesting to see whether the conclusions
drawn above remain valid also under these circumstances.
![[FIGURE]](img111.gif) |
Fig. 4. Modified mass loss `eruption' model (Case C ) obtained by reversing the mass loss rates before and after the `eruption' in the original TT Cyg mass loss history (Fig. 1). Gas and dust velocity at cm (middle) as well as temperature (at and cm; bottom) as a function of time are obtained from two-component radiation hydrodynamics for the mass loss `eruption' model shown in the top panel. For the times labeled `1' to `12', the radial distribution of velocity and density is shown in Fig. 5.
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As before, we applied the DEXCEL code first. The results are
displayed in the lower panels of Fig. 4 and in the left-hand column of
Fig. 5. By design, the conditions before and after the `eruption' are
now reversed: initially, the density of the wind is very low, and so
is the gas outflow velocity,
km s-1, while the
drift velocity is high,
km s-1. During the
`eruption', the gas velocity jumps up to
km s-1, as the
gas/dust coupling becomes very efficient and the drift velocity has
strongly declined to almost zero. After the event, the gas velocity
increases slightly to
km s-1, since the
spectral energy distribution is blue-shifted with decreasing optical
depth of the outflow, leading to a somewhat enhanced radiation
pressure on dust.
![[FIGURE]](img124.gif) |
Fig. 5a-d. Same as Fig. 2, but for the modified TT Cyg mass loss `eruption' scenario defined in Fig. 4. The labeled curves in the upper three panels correspond to times `1' to `12' marked in Fig. 4. The left-hand column displays the results obtained with the DEXCEL two-component radiation hydrodynamics code while the right-hand column shows the corresponding time sequence as obtained with the NEBEL one-component hydrodynamics code using the same , , at the inner boundary at cm as input.
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The gas shell produced by the `eruption' moves outward at an
average speed of
km s-1, the flow
velocity at the center of the shell. Note that this value is
significantly lower than found in the original TT Cyg mass loss
eruption scenario
( km s-1). As before,
the initial velocity plateau in the central parts of the density peak
disappears quickly and gives way to a substantial velocity gradient
across the shell, this time of negative sign. Under these
circumstances the shell is compressed and initially is even narrower
than . Over the whole radial range,
the relative thickness of the shell remains approximately constant at
a rather low value of . It turns out,
however, that this result is again a numerical artifact. Curiously,
numerical diffusion produces a too narrow density structure in this
case.
This becomes clear when recalculating this test case with the NEBEL
code, again using the DEXCEL results at
cm (partly shown in the lower
panels of Fig. 4) as a boundary condition. The NEBEL results are shown
in the right-hand column of Fig. 5, and in Fig. 6.
![[FIGURE]](img130.gif) |
Fig. 6. Radial distribution of gas velocity (top), particle number density (middle) as well as gas temperature and pressure (bottom, solid / dashed) at time yrs (between points 8 and 9), as obtained with the NEBEL one-component hydrodynamics code for the modified TT Cyg mass loss `eruption' scenario defined in Fig. 4. Symbols (+) indicate the numerical grid.
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The propagation velocity of the gas shell produced by the mass loss
event is distinctly larger than that found with DEXCEL,
km s-1. This is
very nearly the same propagation velocity as found before with NEBEL
in the original TT Cyg mass loss `eruption' scenario (compare
Figs. 3 and 6 which show the position of the shell at the same time,
5 867.5 yrs after the end of the mass loss `eruption'). The width
of the shell as a function of radial distance is almost
indistinguishable from the original test case. Obviously, the central
parts of the density peak are not affected by wind interaction; the
width is determined by the duration and outflow velocity of the
`eruption'. Note that in contrast to the DEXCEL results, the action of
the thermal pressure produces a positive velocity gradient at
the center of the shell, which has the same size as in the original
`eruption' scenario (compare the top frames of Figs. 3 and 6).
The wings of the density structure are certainly affected by the
wind properties in front and behind. The reversed wind velocities now
lead to the formation of both a forward and a reverse shock (see
Figs. 5 and 6). The forward shock is stronger because the velocity
jump is larger, and there is a substantial heating associated with
this shock. But the heated region is confined to a thin layer in the
outermost wing where the temperature is as high as 800 K.
Radiative cooling is efficient enough to keep the temperature at a low
constant level ( K) almost
everywhere, and the density jump across the shock by far exceeds a
factor of 4 (which is an upper limit in the "adiabatic" case).
Another NEBEL run without source terms in the energy equation
exhibits the expected behavior: slightly lower outflow velocities,
km s-1, and
essentially the same shell width, but now almost perfectly constant
with radial distance. Heating in the leading shock produces post-shock
temperatures in excess of 6 000 K in the absence of any radiative
cooling. But again the high temperatures are confined to the regions
of very low density in the outer wing of the peak.
Summarizing the results presented in this section, the simulations
leave little doubt that it is indeed possible to produce rather narrow
gas shells of enhanced density through a mass loss event of
sufficiently short duration , as
long as the outflow velocity is constant during the `eruption' and the
stellar wind is highly supersonic. In order to explain the observed CO
emission around TT Cyg, the requirement is
yrs. However, note that our
simulations also indicate that the amount of dust ejected by such an
`eruption' is insufficient to account for the observed excess
dust emission at
100 µm, assuming a
realistic dust-to-gas ratio of (cf.
e.g. Kerschbaum & Hron 1996for the observed spectral energy
distribution of TT Cyg).
3.2. Interacting winds
Interestingly enough, our simulations provide another mechanism
creating thin shells of enhanced gas density, namely the interaction
of two winds of different velocity and density. While analyzing DEXCEL
simulations of the dynamical response of a carbon-rich circumstellar
wind shell to the substantial temporal variations of stellar
luminosity and mass loss rate associated with the final thermal pulses
near the end of the AGB evolution, we discovered that the wind
velocity is an almost bi-modal function of the mass loss rate, as
described in more detail in SSS98.
Briefly, once a critical mass loss rate is exceeded, the coupling
between dust and gas becomes efficient and causes a sudden transition
from a slower, dense, "shock-driven" wind to a faster, less dense,
"dust-driven" wind. Both type of winds carry approximately the same
mass loss rate ( const.). This
behavior inevitably leads to two-wind interaction : The faster
wind in the inner parts of the shell runs into the slower wind in the
outer parts, acting like a snow plow, piling up matter into a thin
shell at the interface between the different kind of winds.
This mechanism is illustrated in more detail in Figs. 7 and 8. The
top panel of Fig. 7 shows the behavior of the mass loss rate during a
typical thermal pulse cycle. Recovering from the mass loss
`interruption' near yrs, the
model's critical mass loss rate ( )
is exceeded at yrs, as
indicated by the abrupt increase of the gas and dust velocity at this
time (middle panel of Fig. 7). According to two-component radiation
hydrodynamics simulations with DEXCEL, the gas velocity `jumps' up by
a factor of 3, from 4 to 12 km s-1, within a time
interval of 10 000 yrs. The reduced density in the inner parts of
the dusty envelope leads to less absorption of stellar radiation and
hence to a slight increase of the dust temperature in the outer
regions beyond cm (lower panel
of Fig. 7).
![[FIGURE]](img159.gif) |
Fig. 7. Top: Mass loss rate as a function of time during a thermal pulse on the upper AGB. Data from stellar evolution calculations with mass loss by Blöcker (1995), for a solar composition star with an initial mass of ending up as a white dwarf with . During the shown time interval, the current stellar mass is reduced from 2.50 to . The next thermal pulse starts at yrs; corresponds to the end of the AGB. Middle: Gas (solid) and dust (dotted) velocity as a function of time at a radial distance of cm as obtained from two-component radiation hydrodynamics calculations based on the stellar evolution sequence shown above. The plotted time interval corresponds to the phase of steadily increasing mass loss rate between two thermal pulses. For the times labeled `1' to `11', the radial distribution of velocity and density is shown in Fig. 8. Bottom: Dust temperature as a function of time at radial distances of cm (upper) and cm (lower) as obtained from two-component radiation hydrodynamics for the same case.
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![[FIGURE]](img169.gif) |
Fig. 8a-d. Same as Fig. 2, but showing the creation and evolution of a shell of enhanced gas density due to two-wind interaction . In each of the upper three panels, there are 11 different curves corresponding to times labeled `1' to `11' in Fig. 7. Data taken from the standard carbon star sequence described in SSS98. The results of the NEBEL one-component hydrodynamics code (shown in the right-hand panels) were obtained by using , , from the DEXCEL two-component radiation hydrodynamics calculations (shown in the left-hand panels) at cm as an inner boundary condition for NEBEL.
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Fig. 8 shows the creation, evolution and propagation of a gas shell
produced by two-wind interaction. Both the DEXCEL (left-hand column)
and the NEBEL (right-hand column) simulation clearly demonstrate that
the resulting density structure is a stable feature traveling to the
outer regions of the circumstellar envelope without loss of identity.
The mass of the shell increases as it keeps sweeping up matter on its
way out. As expected, the results of the two codes differ
quantitatively.
According to DEXCEL, the relative width of the shell is
approximately constant beyond
cm, at a width-to-radius ratio
of . This is very similar to the
result obtained for the mass loss `eruption' scenario C studied
above, where we also found a negative velocity gradient across the
shell, without any indication of a velocity plateau. In contrast,
however, the amplitude of the quantity
( : peak density of the shell) is not
decreasing here with distance but remains approximately constant,
indicating that the mass of the shell grows in proportion to its
radial distance, . More
quantitatively, we measure a shell mass (integral over the range
FWHM) of , a peak density of
g cm-3, and a
density enhancement relative to the `background' of
at
cm, and
,
g cm-3,
at
cm.
A closer inspection of the data reveals that the propagation
velocity of the shell is slightly accelerated, increasing from
=6.6 km s-1 at
cm to
=8.6 km s-1 at
cm. We attribute this
acceleration to the temporal increase of the speed of the inner wind
(cf. middle panel of Fig. 7) and to the fact that the density
structure of the outer envelope does not correspond to a constant mass
loss rate ( ) but exhibits a somewhat
steeper gradient due to the steady growth of the stellar mass loss
rate (factor of 10 over 30 000 yrs, see upper panel of
Fig. 7).
Clearly, these DEXCEL results are affected by numerical
limitations, viz. numerical diffusion (insufficient spatial
resolution, especially in the outer parts of the model) and high
numerical viscosity (in regions of local compression). Application of
the NEBEL code to the same problem shows that the compressed gas shell
is actually expected to be even narrower. The NEBEL results are shown
in the right-hand column of Fig. 8, and in Fig. 9.
![[FIGURE]](img197.gif) |
Fig. 9. Radial distribution of gas velocity (top), particle number density (middle) as well as gas temperature and pressure (bottom, solid / dashed) at time yrs (close to point 9), as obtained with the NEBEL one-component hydrodynamics code for the two-wind interaction scenario based on the stellar evolution sequence with mass loss shown in Fig. 7. Symbols (+) indicate the numerical grid. At this time the parameters of the AGB star are K, , and the gas shell properties are , and .
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In contrast to DEXCEL, the NEBEL simulations suggest that the
relative shell width varies with radius as
(lower right panel of Fig. 8). In
general, NEBEL produces even more narrow shells. At
cm, for example, the
width-to-radius ratio is , at
cm
is less than 0.03 (see also
Fig. 9). This is narrower than the shell widths obtained for all mass
loss `eruption' scenarios studied previously.
As before, we find the propagation velocity of the shell to be
slightly accelerated, increasing from
km s-1 at
cm to
km s-1 at
cm. The average shell
propagation velocity is somewhat higher than indicated by DEXCEL.
However, unlike DEXCEL, NEBEL reveals a velocity plateau at the center
of the shell, indicating the development of a forward and a
reverse shock of roughly equal strength (upper panel of
Fig. 9).
The amplitude of the quantity is
now even increasing with distance; roughly
. This behavior is related to the
fact that the velocity jump across the bounding shock fronts increases
with radial distance, for the reasons mentioned above
( ). Combined with the observation
that const., this again
results in a shell mass that is proportional to the radial distance
from the star, . In this respect,
the results from DEXCEL and NEBEL are consistent.
Summarizing, the results of our simulations covering the phase of
steadily increasing mass loss after a helium-shell flash, strongly
suggest that the mechanism of two-wind interaction is capable of
producing very narrow circumstellar shells of compressed gas
( ) without the need to invoke a mass
loss `eruption' of very short duration. In the presence of molecular
radiative cooling, shock heating of the shell material is negligible
for the parameters considered here (see lower panel of Fig. 9)
In the following section we present a simple analytical model of
two-wind interaction that is suitable to estimate the basic properties
of the resulting shell, given the parameters of the two winds.
3.2.1. A simple analytical model of two-wind interaction
Consider two different, spherically expanding stellar winds: a
"fast" inner wind characterized by a constant mass loss rate
and constant velocity
, and a "slow" outer wind with
parameters and
. It can be shown that the amount of
mass swept up by the "fast" inner wind interacting with the "slow"
outer wind is given by the relation
![[EQUATION]](img215.gif)
where is the distance of the
interaction region from the central star, which increases proportional
with time t (cf. Kwok et al. 1978, Kwok 1983). Since the
situation encountered in the numerical simulations described in the
preceding section may be approximated by
, we simply have
![[EQUATION]](img218.gif)
Substituting typical values from our simulations
( ,
km s-1,
km s-1,
cm; cf. Figs. 7, 8), we find
. This number is in close agreement
with the numerical results from both DEXCEL and NEBEL.
Assuming the collision of the winds to be completely inelastic
(excess kinetic energy is instantly radiated away), the (constant)
propagation velocity of the shell, ,
is given by
![[EQUATION]](img224.gif)
(cf. Kwok et al. 1978, Kwok 1983). If the wind densities are
equal, then and the shell
propagation velocity is the straight mean of the two wind velocities:
![[EQUATION]](img226.gif)
For equal mass loss rates , Eq. (5) reduces to the simple
result that the shell propagation velocity is the geometric mean of
the two wind velocities:
![[EQUATION]](img227.gif)
Substituting the numerical values given above, we obtain
km s-1, while in
the simulations we "measure" a shell velocity of about
7.5 km s-1 (DEXCEL) and 7.9 km s-1
(NEBEL), respectively, at cm,
in general agreement with the analytic estimate. As mentioned before,
both simulations show an accelerated shell velocity, which is related
to the fact that the interacting winds are not really constant, and
therefore the assumption is not
strictly valid. In a simple numerical experiment, we have checked that
NEBEL indeed gives a constant of
the correct magnitude if ,
,
,
are fixed.
Further, Kwok et al. (1978) argue that the width of the shell is
determined by the balance between the internal gas pressure of the
shell, , and the external gas
pressure plus ram pressure of the wind,
. With
,
, and
, the relative width of the
compressed gas shell can be estimated as:
![[EQUATION]](img235.gif)
where is the isothermal sound
speed. For , we obtain
![[EQUATION]](img237.gif)
In this approximation, the relative shell width is independent of
the mass loss rate. Low gas temperature and large velocity difference
( ) favor thin shells (Fig. 10).
Assuming K,
, adopting the numerical values of
and
given above, and making use of
Eq. (7), we obtain a relative width of 0.05, in reasonable agreement
with what is found in the numerical simulations near
cm. According to Eqs. (8) or
(9), we should expect a slight decrease of
with radial distance since
. This is not seen in the DEXCEL
results, but in the NEBEL results, where, however,
. This steeper decline can be
explained by the fact that both the density of the inner wind (the
term ) and the velocity of the inner
wind (the term ) increase with time,
leading to an additional reduction of the shell width (see Eq. (8)).
We have checked that NEBEL gives constant
in the idealized case of two
interacting winds with fixed properties and constant temperature.
![[FIGURE]](img260.gif) |
Fig. 10. Relative shell width according to Eq. (9). Top : as a function of for fixed km s-1, for (dotted), 100 (solid) and 200 K (dashed). Bottom : as a function of temperature for fixed km s-1 and km s-1, assuming a molecular weight of .
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In the framework of the simple analytical model, we can finally
estimate the ratio of gas density in the compressed shell to gas
density in the smooth `background' flow (making use of Eq. (4)) as
![[EQUATION]](img262.gif)
which amounts to a factor of 30 in the above example, in close
agreement with the NEBEL results shown in Fig. 9.
In summary, we conclude that the numerical results of the two-wind
interaction process presented in the preceding section can largely be
understood with the simple analytical model outlined above. The
quantitative comparison of numerical and analytical results again
indicates that the NEBEL code is more reliable than the DEXCEL
code.
3.3. Modeling the circumstellar signature of a typical helium-shell flash
In Sect. 3.2 we have studied the dynamical behavior of the system AGB
star + circumstellar envelope during the phase of steadily increasing
mass loss after the luminosity minimum resulting from the preceding
helium-shell flash. Now we are interested in the consequences of the
shell flash itself. As before, this investigation is based on DEXCEL
simulations of the dynamical evolution of a carbon-rich circumstellar
wind shell of a thermally pulsing AGB star, as described in SSS98. For
reasons to be explained later, we did not use the flash shown in
Fig. 7 but the preceding one occurring near
yrs. Fig. 11 shows the
temporal variation of luminosity and mass loss rate during this
helium-shell flash. Starting from ,
the stellar luminosity begins to decline slowly, before dropping to a
sharp minimum of . Then it takes
only 300 yrs for the luminosity to jump up to
, followed by a more gradual decline
to an extended, deep minimum centered at
yrs where
. According to the mass loss
prescription by Blöcker (1995), the mass loss rate behaves
qualitatively in the same way, but exhibits larger variations since
.
![[FIGURE]](img274.gif) |
Fig. 11. Stellar luminosity (top) and mass loss rate (middle) as a function of time during a thermal pulse on the upper AGB according to stellar evolution calculations with mass loss by Blöcker (1995). Data are taken from the same evolutionary track as before, but refer to the thermal pulse occurring before the one shown in Fig. 7. The lower panel shows the gas (solid) and dust (dotted) velocity as a function of time at a radial distance of cm as obtained from two-component radiation hydrodynamics calculations (DEXCEL) based on the stellar evolution sequence shown above. The thick line (middle and bottom panel) corresponds to the original data, the thin line (-317.005 yrs -315.983 yrs) indicates the modified data used as input for the NEBEL simulations shown in Fig. 12. Times labels `1' to `11' serve as reference marks.
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The concomitant variation of the gas and dust outflow velocity at
cm as calculated by DEXCEL is
plotted in the bottom panel of Fig. 11. As stellar luminosity and mass
loss rate decline, the driving of the outflow by radiation pressure on
dust becomes progressively less efficient and the velocities reach a
minimum at km s-1,
km s-1, where the
wind is assumed to be supported by shock wave pressure (cf. SSS98). It
might even be that the gas falls back onto the star under these
circumstances, but this situation cannot yet be handled by our code.
In any case, this phase lasts for only about 1 000 yrs. It ends
when luminosity and mass loss jump up, leading to an efficient
acceleration of the dusty outflow. The gas velocity reaches a peak
value of 14 km s-1, which is higher than the value
before the onset of the flash (about 10 km s-1). This
period of relatively high velocity is rather short, however. After
another 1 000 yrs, the gas velocity is again down to
3 km s-1, this time for several 10 000 years, as
and
fall to vary low values, and gas and dust decouple completely.
This sequence of events may be viewed as a mass loss
`eruption' which triggers a `storm', i.e a short phase of high
velocity wind. The sharp velocity difference, in turn, inevitably
leads to two-wind interaction and to the formation of a
compressed gas shell. Note that the shell does not consist
entirely of the matter ejected during the `eruption', but also of
material that was ejected earlier, being swept up in the wind
interaction region. Hence, the amount of mass accumulated in the shell
is not directly related to the amount of mass involved in the mass
loss event. Roughly, the gas at the center of the shell was expelled
at the time of peak mass loss.
The formation of a compressed gas shell as a consequence of the
helium-shell flash was not noticed in the original DEXCEL run
documented in SSS98, because the resulting shell was of rather low
amplitude and was washed out quickly by numerical diffusion. Only when
we applied the NEBEL code to this problem, as usual with the
hydrodynamical quantities provided by DEXCEL at
cm as input, the propagation
of a compressed shell through the entire circumstellar envelope was
clearly seen, although the density enhancement
was only moderate and the width of
the shell increased considerably with distance, reaching
at
cm.
In order to further explore the potential of this scenario, we
decided to slightly modify the velocity during the `eruption' phase:
in the time interval -317.005 yrs
-315.983 yrs, we increased the
outflow velocity applied as an inner boundary condition to NEBEL by a
factor of 1.5. Leaving the gas density unchanged, this implies an
enhancement of the mass loss rate by the same factor during this time
span. The modified input data are shown by the thin lines in the lower
panels of Fig. 11. We feel that a factor of 50% can easily be
accommodated within the uncertainties of the model calculations, e.g.
concerning the mass loss prescription and the dust grain
properties.
The NEBEL results for the modified helium-shell flash
scenario are illustrated in Fig. 12. The simulation clearly
demonstrates the efficiency of the helium-shell flash in creating a
large-amplitude, stable density structure traveling to the outer
regions of the circumstellar envelope. The mass of the shell increases
on its way out as a consequence of two-wind interaction.
![[FIGURE]](img286.gif) |
Fig. 12a-d. In the same way as before, this figure illustrates the creation and evolution of a shell of enhanced gas density as a consequence of the (modified) helium-shell flash shown in Fig. 11. In each of the upper three panels, there are 11 different curves corresponding to times labeled `1' to `11' in Fig. 11. These results were obtained with the NEBEL one-component hydrodynamics code using , , from the DEXCEL two-component radiation hydrodynamics calculations at cm (shown partly in the lower panel of Fig. 11) as an inner boundary condition. Artifacts beyond cm should be ignored.
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The NEBEL simulations suggest that the relative shell width is
essentially constant with radial distance:
(lower panel of Fig. 12). Note that
this number is in close agreement with the observed relative width of
the CO shell around TT Cyg (Olofsson et al. 1998, 2000).
The average propagation velocity of the compressed shell is of the
order of 14 km s-1, while, according to Olofsson et
al. (1998, 2000), the expansion velocity of TT Cyg's CO shell is
12.6 km s-1, a remarkable coincidence. A closer
inspection of the data reveals that the propagation of the shell is
slightly decelerated, decreasing from
km s-1 at
cm to
km s-1 at
cm. We attribute this
deceleration to the loss of momentum as a consequence of sweeping up
`slow' gas at the outer edge of the shell at decreasing support from
the `fast' wind at the inner edge of the shell. It is important to
note that we again find a velocity plateau at the center of the
shell (see also upper panel of Fig. 13), which is a typical
feature of supersonic wind interaction (double-shock structure). This
is consistent with the observational fact that the velocity dispersion
indicated by the line width of CO emission from TT Cyg's shell is
very low, of order of only 1 to 2 km s-1 (Olofsson et
al. 1996, 2000).
![[FIGURE]](img307.gif) |
Fig. 13. Radial distribution of gas velocity (top), particle number density (middle) and gas temperature / pressure (bottom, solid / dashed) at time yrs (between points 5 and 6), as obtained with the NEBEL one-component hydrodynamics code for the modified helium-shell flash scenario based on the stellar evolution sequence with mass loss shown in Fig. 11. Symbols (+) indicate the numerical grid. At this time the parameters of the AGB star are K, , and for the gas shell we measure , .
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The amplitude of the quantity is
decreasing somewhat with distance, indicating that the mass of the
shell grows in a non-linear way with radial distance. At
cm, we measure a shell mass
(integral over the range
FWHM) of
, a peak density of
g cm-3, and a
density enhancement relative to the `background' of
, while
,
g cm-3,
at
cm. Again, it is worth
mentioning that these numbers are in general agreement with the
estimate of the mass of the CO shell around TT Cyg and the gas
density density within the shell as given by Olofsson et al. (1998,
2000): and
g cm-3.
Shock heating of the shell material seems to be negligible in the
presence of molecular radiative cooling, as may be seen from the
undisturbed temperature profile across the shell shown in the lower
panel of Fig. 13. The kinetic temperature of the compressed shell
equals the dust temperature, K
at cm. This is consistent with
the finding by Olofsson (2000),
K, in particular if we assume
the material to be clumpy (see below). Since the temperature is
uniform across the shell, pressure and density gradients always have
the same sign, and hence there is no reason for the shell to become
Rayleigh-Taylor unstable.
We have performed similar calculations for the subsequent
helium-shell flash (depicted in Fig. 7). Here the temporal variations
of luminosity and mass loss rate are qualitatively similar, but occur
on a somewhat higher mean level; the peak mass loss rate is almost a
factor of 2 higher. In consequence, the outflow velocity is no longer
a monotonic function of the mass loss rate during the `eruption' as in
the previous helium-shell flash (see Fig. 11). Rather, the outflow
velocity decreases sharply at the time of maximum
, because the radiation pressure on
dust is momentarily reduced due to the high optical depth of the dust
shell produced by the heavy mass loss. Under these circumstances, the
rapid velocity variations during the flash-induced mass loss
`eruption' eventually lead to the formation of a double shell .
We have not yet studied this more complex case in detail. We just
point out that, evidently, the circumstellar signature of a
helium-shell flash depends sensitively on the amplitude of
(t) and
(t) during the flash, which in turn
depends on the stellar core mass and the evolutionary stage on the
AGB.
In summary, the results of these simulations covering the
helium-shell flash and the ensuing phase of rapidly decreasing mass
loss, clearly demonstrate that the sharp peak in luminosity and mass
loss rate associated with the occurrence of a helium-shell flash
triggers a short period of strongly enhanced wind speed. This, in
turn, must lead to two-wind interaction which has the potential to
produce very narrow circumstellar shells of compressed gas
( ,
). Note that it is not necessary to
invoke unknown physical processes for this scenario to operate. All
that is needed is some plausible fine-tuning.
© European Southern Observatory (ESO) 2000
Online publication: May 3, 2000
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