Fig. 8
Sonic Mach number (upper panel), normalised CR pressure (middle panel), compression ratio and factor proportional both to Eesc,d and Eloss for parallel shocks (grey and black lines, respectively, in lower panel) as a function of the temperature for x = 0.3, η = 10-5; U = 40 km s-1 (solid lines), U = 80 km s-1 (dashed lines), U = 120 km s-1 (dotted lines), and U = 160 km s-1 (dash-dotted lines).
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