# Moderately Resolved High Mach Number Cooling Test

**Note: the plots are in log-linear so sharp dips are from negative values.**

This plot shows the steady state solution in black for a shock with a Mach number of 50. The cooling curve is a simple power law with an exponent of 2 and a coefficient of 1.23786e-34. The steady state is then put into the code as initial conditions with a resolution of 102 zones across the 2.5e17 cm (only 2 across the input cooling length). The red curve shows the state of the shock after 1500 years and 500 time steps. The epsilons were all set to zero and the time step was a factor of ten smaller than the cooling time.