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What is C-D Nozzle Shock Analysis and Flow Patterns about?

This document discusses different flow conditions in a converging-diverging nozzle: - Shock is formed in the diverging section when P0=20 psi and 30 psi - Shock is formed at the exit when P0=35 psi, with pressures and mach numbers calculated - The case is overexpanded with A/At=1.2, M design =1.53414, with pressures, shock angle, and deflection angle calculated - No shock is formed when M design =1.53414 and back pressure matches calculated pressure

Author

Patnala Susmitha

Language

EN