Table 1: Properties of a radiative shock for gas with a ratio of specific heats, $\gamma =5/3$ .
M $\rho_{\rm s}/\rho_{\rm0}$ $\rho_{\rm c}/\rho_{\rm0}$ $T_{\rm s}/T_{\rm0}$

1.4 1.58 3.27 1.39

2.0 2.29 6.67 2.08

3.0 3.00 15.0 3.66

5.0 3.57 41.7 8.68

10.0 3.88 167 32.1

20.0 3.97 667 126

40.0 3.99 2667 501

**Table 1:** Properties of a radiative shock for gas with a ratio of specific heats, $\gamma =5/3$ .
M	$\rho_{\rm s}/\rho_{\rm0}$	$\rho_{\rm c}/\rho_{\rm0}$	$T_{\rm s}/T_{\rm0}$
1.4	1.58	3.27	1.39
2.0	2.29	6.67	2.08
3.0	3.00	15.0	3.66
5.0	3.57	41.7	8.68
10.0	3.88	167	32.1
20.0	3.97	667	126
40.0	3.99	2667	501

Source LaTeX | All tables | In the text

	1 Introduction
	2 Properties of low Mach number shocks
	3 Hydrodynamical simulations
	4 Discussion
	5 Summary
	References