Investigation of the Mach reflection associated with a steady two-dimensional overexpanded nozzle flow. The conditions of occurrence of triple point shock configuration are described, and Mach reflection configurations for two values of the incident shock are presented, along with the Mach stem height variation for different Mach numbers under conditions of different pressure ratios.
No takes yet. Share an insight, caveat, or question.
Chow et al. (1972) studied this question.
Synapse has enriched 5 related papers. Consider them for comparative context: