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Astron. Astrophys. 327, 392-403 (1997)
3. Results
We consider several models defined by combinations of input
parameters controlling the solutions of Eqs. (26)-(30), They belong to
three different groups. First of all, one can choose between the
equatorial and the polar solar wind. In the former case the initial
values of hydrodynamic parameters at 1 AU are (Schwenn, 1990):
![[EQUATION]](img53.gif)
while those of the polar wind are (McComas et al., 1995):
![[EQUATION]](img54.gif)
The pressures above correspond to temperatures of
K and K, respectively.
The pressures of the cosmic rays components are the same in both
models:
![[EQUATION]](img57.gif)
The pressure of galactic cosmic rays is close to the value of
, typical for the inner heliosphere (Jokipii,
1990).
The next set of parameters determines the pick-up ion source terms
(Eqs. (5)-(7)). At the solar minimum the densities of neutral
components of LISM and their ionization rates at 1 AU are (Lee,
1995):
![[EQUATION]](img59.gif)
The above values correspond to the lower limit of the referenced
values. The recent Ulysses data (Witte et al. 1993) suggest that the
density values may even be more than 2 times larger. Also at solar
maximum the ionisation rate can significantly increase. Therefore, we
will use also the following values:
![[EQUATION]](img60.gif)
The last group of parameters consists of the diffusion coefficients
for the galactic and anomalous cosmic rays, .
Unfortunately, it is not possible within the framework of the present
model to calculate self-consistently the diffusive coupling between
the ambient medium (plasma and magnetic field) and the cosmic rays.
Moreover, since the diffusion coefficients averaged over the spectrum
of energies of each kind of cosmic rays are not well known,
must in fact be treated as free parameters of
the model. It is well known that the diffusion coefficient is a
function of the turbulence level and of the
magnetic field B itself; the diffusion in the direction
perpendicular to the field is generally less efficient than the
diffusion along the field ( ). As the upwind
field decreases with r, we assume that the upwind diffusion
coefficients increase:
![[EQUATION]](img65.gif)
In the ecliptic plane, where the field is azimuthal, the
cross-field diffusion is appropriate; in the polar heliosphere the
parallel diffusion coefficient should be taken into account. In the
post-shock region both the magnetic field ( ) and
the turbulence level increase, but, as the functional dependence of
K on the field and on the number of scattering centers is not
fully known, the value of the downwind diffusion coefficient is
difficult to specify. In order not to multiply the amount of numerical
results, in this paper we assume that the downwind diffusion
coefficients, , are constant and equal to the
upwind values at the shock. According to Potgieter et al. (1987), the
diffusion coefficient is proportional to the thermal velocity of
diffusing particles, so that , corresponding to
particles with energy 10 MeV, is assumed to be 10 times smaller than
, which describes particles in the GeV energy
range. We follow this prescription in calculating the equatorial
models, and represent by linear functions with
moderate ( , ) and steep
( , ) gradients. The values
of and are chosen in
that way that the average value of in the
upwind region (i.e. over 100 AU), is in both cases similar and amounts
to . In the polar wind, the average value must
be increased to avoid singularities in the solutions. To simplify the
considerations we take the constant value of ),
which is probably the upper limit of possible coefficients, and tune
the value of to obtain the physically
meaningful solutions.
All models are summarized in Table 1.
![[TABLE]](img80.gif)
Table 1. Models: input parameters and main results
Two other quantities, important in evaluating the obtained
solutions, are the pressure of galactic cosmic rays far away from the
Sun ("at infinity") and the pressure of the local interstellar medium.
According to Lee & Axford (1988), the LISM pressure should be in
the range , the upper value being more likely.
These values are uncertain mainly due to our very limited knowledge
about soft (MeV) galactic cosmic rays in the LISM. In consequence, one
can argue for either subsonic or supersonic LISM (Zank et al, 1996b).
For the galactic rays pressure, we assume
(Axford, 1985).
We have found that the correct value of the LISM pressure at the
heliopause is obtained for only a narrow interval of
, which, however, changes for different
. Values of smaller than
the lower limit of the mentioned interval result in an increase of the
downwind ACR pressure with distance, which corresponds to the source
at infinity, not at the shock. The large , on
the other hand, forces a steep negative gradient of the ACR pressure
at the shock, which, in consequence, leads to unphysical, negative
values of the ACR pressure in the downwind region (Fig. 1).
3.1. Equatorial models
The results of four equatorial models are showed in Figs. 2-5.
Three quantities: velocity, galactic and anomalous cosmic rays
pressure are plotted here as functions of the heliocentric distance
for the assumed shock positions at 65, 80, and 95 AU. The presented
solutions correspond to the largest possible
still yielding a non-negative ACR pressure in the downwind region.
![[FIGURE]](img81.gif) |
Fig. 2. Velocity v and cosmic rays pressures and as functions of a distance for model 1. Three different positions of the shock are indicated by dotted lines; from each one of them the downstream intergration starts and results in a different profile of the considered quantities. The production efficiency is chosen for each shock as a maximum possible value from the range (0,0.15) still yielding a nonnegative ACR pressure downstream of the shock. It is equal 0.0, 0.01, and 0.06 for the shock at 65, 80, and 95 AU, respectvely.
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![[FIGURE]](img84.gif) |
Fig. 3. The same plot as in Fig. 2 for model 2. The values are 0.0, 0.04, and .
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![[FIGURE]](img90.gif) |
Fig. 4. The same plot as in Fig. 2 for model 3. The values are 0.0, 0.01, and 0.05.
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![[FIGURE]](img96.gif) |
Fig. 5. The same plot as in Fig. 2 for model 4. The values are 0.0, 0.04, and .
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Velocity. As the result of mass loading the upwind velocity
decreases with distance, first linearly, then with an increasing
gradient. Clearly, the models 3 and 4, with a smaller pick-up ion
production also show a smaller velocity decrease. The steeper gradient
of the diffusion coefficients (models 2 and 4) results in a very
efficient slowing down of the flow; velocities at the most distant
shock position (95 AU) are quite low, about 200 km/s. The velocity
profiles for AU show a strong precursor
structure; in each case one observes a thick region of a large
negative velocity gradient, that can be interpreted as a precursor of
weak shock. In the inner heliosphere the dominant terms in Eq. (24)
determining the velocity profile are: the gas pressure gradient and
the momentum exchange with neutrals, while near the shock the cosmic
rays pressure and the momentum loss to the neutrals dominate.
GCR pressure. The galactic cosmic rays pressure increases
monotonically, with a faster rate in the upwind, and more slowly in
the downwind region. The obtained GCR pressure is, for all models, in
the range , in good agreement with the canonical
value of - . The more
distant the shock, the larger the GCR pressure at the heliopause
(i.e., practically, "at infinity").
ACR pressure. The anomalous cosmic rays pressure shows the
largest variations among different models. Also, for a given model,
the ACR pressure at the shock is very sensitive to the shock position.
This follows from a strong dependence of on the
velocity; as was explained earlier, v varies significantly near
the shock. One can say also that the ACR diffusion is most efficient
at places where the density of scattering centers (solar wind) varies
most, i.e. in a heavily mass loaded wind, close to the shock. The form
of in the downwind region is, to a large extent,
determined by ; this parameter appears in the
conservation equation (21) and influences the post-shock value of
- the intial condition for the downwind
integration. One can see (Table 1), that the shock at 65 AU allows for
a very small ( )
regardless of the model. For AU one gets
, the upper limit obtained for models with a
steep gradient of . Finally, large
values ( ) are still
acceptable for the most distant shocks (at 95 AU).
Gas pressure and magnetic pressure. Gas pressure dominates
the overall pressure near the Sun. It falls down rapidly with the
distance, following the density variation. At the shock, P
shows a step-like increase and then decreases slowly towards the
heliopause (Fig. 6). This pattern is very similar for all models
considered, and the quantitative differences are not large. At the
heliopause P amounts to and is smaller
than . The magnetic pressure at 200 AU is larger
than P by a factor ranging from 2 ( AU,
models 3 and 4) up to 15 ( AU, models 1 and 2).
The sum of both pressures, which should balance
at the heliopause, vary between
, depending on the model and
. In general, it decreases with the shock
distance and is larger for a smaller pick-up ion production rate. In
Fig. 6 we also show a profile of the polytropic pressure variation,
that starts from the same value as P at 1 AU. Even if the
difference between the polytropic and nonpolytropic pressure at the
shock is somehow exaggerated here (the density profile in the
polytropic model would be different from the value of
obtained in our model), one still may come to
the conclusion that quantitative results obtained from the polytropic
models must be treated with great caution.
![[FIGURE]](img108.gif) |
Fig. 6. Gas pressure P and magnetic pressure as functions of distance for model 1. The shock is set at 80 AU. The polytropic pressure (dotted line) is shown for comparison with P obtained from a nonpolytropic model.
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Density. The source term in Eq. (26) increases the solar
wind density above the value that would be obtained for a mass
conserving flow. For an efficient mass loading (models 1 and 2) the
increase amounts to 10% at 80 AU and 12% at 95 AU. The models with low
source-rate of pick-up ions show an increase of about 2-3%.
Compression ratio. For a single-fluid, classical shock with
one obtains . As
mentioned earlier, two opposite effects included in our equations can
modify this canonical value: production of ACRs leads to an increase
of q, the mass loading of the wind with pick-up ions results in
q smaller than 4. In Fig. 7 we present the compression ratio as
a function of obtained for four equatorial
models and two values of : 0.05 and 0.15 (Note,
that only for AU ( ) and
for AU ( ) some of our
models give meaningful solutions for in the
downwind region). For , the mass loading effect
dominates the ACR production and the resulting q is smaller
than 4. It can be as small as 2.7-2.8 for a distant shock, small
( ), and the model with
the efficient pick-up ion source.
![[FIGURE]](img122.gif) |
Fig. 7. Shock compression ratios q as functions of the shock distance for the ecliptic solar wind models: 1 ( ), 2( ), 3( ), 4( ), and for two values of .
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3.2. Polar models
Similarly as for the equatorial models, we consider two different
production rates of pick-up ions. The main difference with respect to
the equatorial case is a change of the cosmic rays diffusion
coefficients. An attempt to use the same values as for the equatorial
models was unsuccessful: either the obtained
was too large, or, what was even worse, the solutions of (26)-(30)
appeared to be singular in the upwind region. Therefore, we had to
change and . An increase
of to about ensures
that the obtained is approximately correct. In
order to avoid singularities in the solution,
must be larger than . The above numbers
correspond to the upper limits of diffusion coefficients considered in
the literature. In what follows, we will present the results obtained
for a constant and
varying from to (Figs.
8-11). The ACR pressure close to the shock is extremly sensitive to
the value.
Since the expected distance to the heliopause should be larger in the
polar than in the equatorial plane (in the direction towards the
stagnation point), we will now consider in the
range 80-120 AU.
![[FIGURE]](img138.gif) |
Fig. 8. The same plot as in Fig. 2 for model 11. The values are 0.0, 0.01, and 0.04.
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![[FIGURE]](img140.gif) |
Fig. 9. The same plot as in Fig. 2 for model 12. The values are 0.0, 0.07, and .
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![[FIGURE]](img144.gif) |
Fig. 10. The same plot as in Fig. 2 for model 13. The values are 0.0, 0.01, and 0.10.
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![[FIGURE]](img146.gif) |
Fig. 11. The same plot as in Fig. 2 for model 14. The values are 0.0, 0.04, and .
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From the physical point of view, the two important differences of
the polar flow as compared with the equatorial one are: (i) the wind
is faster in the upwind region, and (ii) the magnetic pressure in the
downwind region vanishes. The magnetic pressure stabilizes the flow;
in the equatorial models the upwind solutions are always regular,
while the polar models almost always fail before reaching the
heliopause: either the velocity becomes negative or the denominator in
(27) goes to zero. One could argue that behind the shock the magnetic
field is no longer parallel to the shock and, therefore, the magnetic
pressure is not negligible there. However, we decided not to introduce
the magnetic pressure and follow the downwind solutions as far as
possible. At the point where the calculations are terminated, the
solar wind and the GCR pressures are practically constant and can be
extrapolated to the heliopause in order to be compared with
and .
Velocity. The polar models show a relatively larger decrease
of velocity on the way from 1 AU to the shock than the equatorial
models, but this effect results from the larger distance to the shock,
not the larger velocity gradient. Again, the models with a less
efficient pick-up ion source show a smaller velocity decrease. The
impressive slowing down of the solar wind at 100-120 AU in models 12
and 14 follows from a very steep ACR pressure gradient.
GCR pressure. The galactic cosmic ray pressure shows similar
profiles as in the equatorial cases, it is, however, larger at the
heliopause ( ) because more distant shocks
provide an extra room for its increase. The value of
can be easily decreased by a different choice
of initial conditions or .
ACR pressure. The anomalous cosmic ray pressure is very
sensitive to the diffusion coefficient. Its moderate change, from
to , yields a dramatic
increase of the ACR pressure at the shock (approximately a factor of
4). Such an effect has not been observed for equatorial models, but
could not be excluded - we have not tried to explore the whole
parameter space.
Gas pressure and density. The upwind variations of the
pressure are similar in form to the equatorial profiles. The magnetic
pressure is zero, therefore downstream of the shock only the gas
pressure contributes to the pressure balance at the heliopause. Its
value at the heliopause (or at the point where calculations are
stopped) decreases with the distance of the shock; for shocks at
80-100 AU, P is equal to , which is too
large as compared with the expected LISM pressure. From this point of
view only the shocks at 110-120 AU are acceptable - they yield
pressures of . For models with large anomalous
cosmic ray production at the shock (12 and 14), the upstream density
shows an interesting feature - it decreses, as one could expect, to a
distance of 100 AU but then starts to increase, forming a kind of wall
in front of a distant (very weak) shock ( AU).
This increase is, of course, correlated with a very steep velocity
decrease in this region. The mass loading effect amounts to 11-18% at
AU for the efficient ionization (models 11,
12), but is 3-4 times smaller for models 13 and 14.
Compression ratio. Perhaps the most interesting issue is an
appearance of very weak shocks for models 12 and 14. The value of
q can be as small as 1.6-1.8 (Fig. 12). In fact, such
structures are very close to a shock-free transition from one flow to
another.
![[FIGURE]](img142.gif) |
Fig. 12. Shock compression ratios q as functions of the shock distance for the polar solar wind models: 11 ( ), 12( ), 13( ), 14( ), and for two values of .
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© European Southern Observatory (ESO) 1997
Online publication: April 8, 1998
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