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This paper discusses the flow characteristics through a convergent-divergent nozzle, focusing on the analysis of mass flow rate in relation to pressure ratio, area ratio, and Mach number. It covers various flow regimes including subsonic, sonic, supersonic, and hypersonic flows, and provides mathematical equations to calculate mass flow rates under different conditions. The study concludes with numerical results derived from the equations, demonstrating the relationship between mass flow rate and the parame

Author

Prashant Kumar

Language

EN