Figure 6: MPEG movie showing the
evolution of the density distribution for the shock heating
problem with an inflow velocity
in Cartesian
coordinates. The reflecting wall is located at . The adiabatic index of the
gas is 4/3. For numerical reasons, the specific internal energy
of the inflowing cold gas is set to a
small finite value ( ). The final frame of the movie also shows the analytical solution (blue lines).
The simulation has been performed on an equidistant grid of 100 zones.
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