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Astron. Astrophys. 325, 857-865 (1997)
5. Tests
Any form of artificial viscosity must be able to form and propagate
a shock. The modification of the artificial viscosity, Eq. (13) and
(16), is tested in a shock forming test and compared with the standard
artificial viscosity, Eq. (6), introduced by Monaghan and Gingold
(1983). The ability of the modified artificial viscosity to compress
the gas without viscous deceleration and heating has also been tested
in a homologous compression of a gas sphere. The test constructed by
Evrard (1988) is used to study the differences between the artificial
viscosities in a gravitational collapse of an initially cool gas
cloud.
The number of particles is varied between 8192 and 16384, and the
number of neighbours for each particle is 64, so that h is varying in
time and space. In the equation of state the adiabatic index is
to model an ideal monoatomic gas. Dimensionless
units are used to keep the quantities in the model around unity, where
the gravitational constant . In a model the
total mass , the typical length
and time , which relates
to the gravitational constant as . The real
quantities of the model can be calculated by inserting the
corresponding quantities in the desired unit system.
5.1. Shock formation test
A box with dimensions is used. Periodic
boundary conditions are applied in the x - and y
-directions. At the ends of the tube, and
, no boundary conditions were applied, so the
particles are allowed to move away from the tube. Their velocities are
however low compared with the velocity of the shock and do not affect
the shock model. The 16384 particles are ordered in a cubic centered
grid, such that 8192 particles are distributed at
, and the rest at . With a
total mass of 1.0 mass units the density distribution is
![[EQUATION]](img85.gif)
The initial thermal energy density is set to 0.01, and the
particles have no initial velocity. A shock is formed at the
discontinuity at , which propagates to the
right. This is a rather weak shock, which is a better test than a
strong shock. The reason is that here the particle velocities are not
much larger than the sound speed, because if they are the standard and
modifies artificial viscosity become similar. Fig. 1 shows the shocks
at with the standard artificial viscosity, Eq.
(6), and Fig. 2 using modified artificial viscosity, Eq. (13) and
(16). A comparison between Fig. 1 and
2 shows that the shocks formed
by the two versions of artificial viscosity are similar, so that the
modified artificial viscosity is able to work in the same way as the
standard artificial viscosity.
![[FIGURE]](img2.gif) |
Fig. 1a-c. A shock in a shock tube with standard artificial viscosity, Eq. (6), which was formed by the density discontinuity described in Eq. (20). a shows at time the velocity distribution, b the pressure and c the density distribution.
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![[FIGURE]](img4.gif) |
Fig. 2a-c. Same as
Fig. 1, but with modified artificial viscosity, Eq. (13) and (16).
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5.2. Homologous compression of a gas sphere
The ability of the modified artificial viscosity, Eq. (13) and
(16), to handle compression of a gas realistically is tested.
Initially 8192 particles are distributed unifomly in a sphere with
radius on a slightly disturbed cubic centered
grid. There are no boundary conditions applied, but there is an
initial velocity distribution directed towards the origin according
to
![[EQUATION]](img88.gif)
where is a constant and
the position in the sphere. The particles are
initially isothermal with a thermal energy density of
, and with a total mass of
, which gives an initial density of
. The sum of the total kinetic,
, and thermal, , energies
is
![[EQUATION]](img94.gif)
Assume that the compression is adiabatic, so that Poisson's
equation,
![[EQUATION]](img95.gif)
is valid. From the equation of state, , and
the adiabatic index, , it follows that
![[EQUATION]](img97.gif)
If it is assumed that all kinetic energy is converted to thermal
energy at maximum compression, the thermal energy density at this
point is
![[EQUATION]](img98.gif)
This gives a density and radius of the compressed gas sphere as
![[EQUATION]](img99.gif)
This zeroth order approximation is useful to compare with
calculations with different forms of artificial viscosity. The initial
conditions also have the advantage that no artificial viscosity is
needed to prevent interparticle penetration. A small initial pressure
is sufficient to decellerate the particles to zero and prevent them to
move through the origin. The results from the test with modified
artificial viscosity can therefore not only be compared with the
analytical approximation Eq. (25), but also with a model without any
artificial viscosity. The energy curves from such a comparison are
shown in Fig. 3. In Fig. 4 the density distributions at time
are compared.
![[FIGURE]](img101.gif) |
Fig. 3. The energy curves for the homologous compression of a gas with different forms of artificial viscosity. The solid line represents the compression without any artificial viscosity at all, the dashed the modified artificial viscosity, Eq. (13) and (16), and the dotted the standard artificial viscosity, Eq. (6). The curves that decline in the beginning represent the kinetic energies for the three models, those that rise represent the internal and the uppermost straight curves represent the total energy.
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![[FIGURE]](img35.gif) |
Fig. 4a-c. The density distribution for the homologous compression of the sphere at maximum compression without any artificial viscosity in a, with standard artificial viscosity in b, Eq. (6), and modified artificial viscosity, Eq. (13) and (16) in c. The results in a and c are plotted with the same scale, while another scale must be used in b. The solid line in a and c represent the zeroth order theoretical estimate from Eq. (26) at maximum compression where the radius is 0.029 and the density 10000.
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The heating in the case with standard artificial viscosity, Eq.
(6), starts immediately, because it depends on the relative
velocities, while the heating without artificial viscosity and with
the modified artificial viscosity is negligable until
. The modified artificial viscosity has a little
less steep energy curve compared with the case without artificial
viscosity, but gives an almost a compressed gas as without artificial
viscosity as seen in Fig. 4. The true density distribution is not
known, but the zeroth order approximation from Eq. (25) gives
approximately the same size as the model without artificial
viscosity.
5.3. The Evrard gravitational collapse
The initial conditions are those from Evrard (1988), which is a
isotherm sphere at rest with a thermal energy density of
, radius and mass
. Initially 8192 particles are distributed
uniformly in a sphere with radius on a slightly
disturbed cubic centered grid with a density distribution of
![[EQUATION]](img106.gif)
Standard, Eq. (6), and modified artificial viscosity, Eq. (13) and
(16) are tested with this model and compared with each other.
Due to the cold initial state the sphere begins to collapse. Since
the central part is more dense than the outer payers, the collapse is
more rapid around the origin. A high central pressure and density is
build up, and the central parts starts to expand at
. Where the expanding parts meet the infalling
gas, an outward propagating shock front forms. Eventually the gas
reach a virial equilibrium.
The total energies are shown in Fig. 5a and b. The curves are more
shallow in Fig. 5a, where standard viscosity was used, than in
Fig.
5b. In Fig. 6 the velocity, density and pressure distributions are
plotted with standard artificial viscosity at
when the shock is formed. This can be compared with the results from
modified artificial viscosity for the same quantities which are shown
in Fig. 7. The main difference between these models are the sharper
gradients with modified artificial viscosity. This is an effect of the
ability to compress the gas with modified artifial viscosity. The
infalling gas is allowed to move inwards without decelleration until
it meets the shock front.
![[FIGURE]](img45.gif) |
Fig. 5. The energy curves for the Evrard gravitational
collapse using standard artificial viscosity, Eq. (6), represented by a dashed line, and modified
artificial viscosity, Eq. (13) and (16), represented by a solid line. The uppermost curves
represent the internal thermal energy, the next the kinetic, the straight line the total and the
two curves below the others' the potential energy. The solid line is from an accurate
one-dimensional PPM calculation at from
Steinmetz & Müller (1993).
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![[FIGURE]](img69.gif) |
Fig. 6a-c. The velocity, density and pressure distributions for the Evrard gravitational collapse using standard artificial viscosity, Eq. (6). The radial velocity, density and pressure are plotted at t=0.8. The crosses are values at t=0.77 are results from an accurate one-dimensional PPM calculation from Steinmetz & Müller (1992).
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![[FIGURE]](img71.gif) |
Fig. 7a-c. Same as
Fig. 6, but with modified artificial viscosity, Eq. (13) and (16).
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© European Southern Observatory (ESO) 1997
Online publication: April 28, 1998
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