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Numerical calculations have been made about shock reflection processes in ionizing argon on the end wall of a shock: tube. The two-step Lax-Wendroff scheme was employed to solve time-dependent one-dimensional inviscid flow problems for ionizing gases. Complicated flowfields were found to occur due to interactions between ionization relaxation processes and reflected shocks. Calculations were performed for three cases: incident-shock Mach number M s = 16 and initial pressure p 1  = 1 torr; Ms = 14 and p 1  = 3 torr; M s = 12 and p 1  = 5 torr.

Numerical Calculations on Reflection Processes of Ionizing Shocks on the End Wall of a Shock Tube