The Short Characteristics tracer (e.g. Raga, 1999) is used to trace out rays from a source in a causal manner, calculating the optical depth to a cell by interpolating between (previously calculated) optical depths to neighbouring cells closer to the source. Given that we are ignoring diffuse radiation (the On-the-Spot approximation) the diffusion in the ray-tracer is not significant, and is minimized using the weighting scheme given by Mellema (2006).
When the photo-ionisation time is short compared to other time-scales
(cooling, recombination, and collisional ionisation times) the
microphysics equations become difficult to solve explicitly so we
adopt a dual approach. In cases of weak photo-ionisation, we use an
explicit 5th order Runge-Kutta technique with adaptive step-size to a
given relative accuracy (Press, 1992). For strong photo-ionisation we
integrate explicitly until the Hydrogen ion fraction, , satisfies
, and then analytically integrate the equations assuming a
constant electron density (as described in Mellema 2006),
with bisection substepping to convergence (typically
substeps).
For both of these methods we use a relative error tolerance of 0.001.
This algorithm also calculates the time-averaged optical depth through
the cell
, which is then used by subsequent cells in the
ray-tracer. Mellema (2006) use a simple time average of
, however we use a time average of
since this gives a time average of the fraction of photons passing
through the cell. This can be easily seen in the (extreme) case of an
optically thick cell which is photo-ionised ``rapidly'' half way
through a unit timestep, so that
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(1.1) |
We use monochromatic radiation with a hydrogen photo-ionisation
cross-section of
and an energy gain
of
eV per photo-ionisation. Collisional ionisation rates are
calculated with fitting functions from Voronov (1997), and radiative
recombination (Case B) rates using the tables calculated
by Hummer (1994). The difference between planar radiation and
radiation from a point source can be quite significant if the size of
the computational domain is comparable to the distance to the source.
The rocket effect is weaker further from a point source due to the
inverse square law, which may extend the lifetime of any structures
that form. This effect can, however, reduce the length of such
structures since the intensity of the radiation is higher at their
heads. In the case of M16, the heads of the pillars are about
pc
from the brightest star, and they are about
pc long, so the flux
dilution is more than a factor of 2 along their length. We therefore
use a point source in this work.
Jonathan Mackey