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Astron. Astrophys. 328, 121-129 (1997) 4. 3D numerical simulationsThe expansion of gas layers around OB associations may be described as a blastwave propagating into the interstellar medium (Ostriker & McKee, 1988; Bisnovatyi-Kogan & Silich, 1995). A multi-supernova remnant follows an initial quasi-adiabatic stage, driven by the thermalized energy of the supernova ejecta. The energy from each new supernova is released within the remnant created by all previous stellar winds and explosions. Once the radiative losses become important a thin and cold shell forms at the outer edge of the cavity, which is filled by the hot medium. Due to its supersonic speed the shell continues to collect the ambient medium and it slows down to velocities comparable to the random motion of the interstellar medium. Since the radius of the shell R is much larger than the
thickness of it, the thin layer approximation considered by Sedov
(1959) and developed by Kompaneets (1960) and Bisnovatyi-Kogan &
Blinikov (1982) can be applied. This approximation has been adopted in
two dimensional models of expanding shells by Tenorio-Tagle &
Palou Here, the 3D computer model of an expanding infinitesimally thin
shell as described by Ehlerova &
Palou 4.1. Initial conditionsAt an initial time The internal pressure where 4.2. Energy inputs from sequential supernovaeDuring their evolution, SN explosions supply energy to the bubble.
The rate of energy input is given by In previous simulations (Ehlerova &
Palou In this paper, the internal thermal energy is evaluated at every timestep, and subsequently the pressure and temperature are derived. The internal energy of a bubble changes due to:
where where 4.3. Integration schemeIn the 3D numerical simulations, the shell is divided into
where The mass conservation equation gives the increase of mass m
as long as the expansion velocity component normal to the shell,
After the expansion becomes subsonic, the mass m of an element is constant. The momentum conservation equation (21) and mass conservation equation (22) are solved numerically together with the equations for the internal energy (20) using finite timesteps. An adaptive step-size control scheme is used, which will be described elsewhere. The main advantages of this scheme are the known accuracy of the integrated quantities and the savings of the CPU time, particularly in the subsonic stage where the timestep can be large without loosing the accuracy. ![]() ![]() ![]() ![]() © European Southern Observatory (ESO) 1997 Online publication: March 24, 1998 ![]() |