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Design & Simulation of Mach 8 C-D Nozzle by siriusaam is a document available to read on EtoBox.
The project focuses on designing and simulating a Convergent-Divergent Nozzle to achieve an exit Mach number of 8, utilizing ANSYS Fluent for analysis under laminar and turbulent flow conditions. Two nozzle geometries, linear and bell-shaped, are compared for their impact on flow behavior, with findings indicating that the bell-shaped design offers smoother expansion and reduced shock formation. Key results highlight the importance of nozzle geometry and flow conditions in optimizing performance for high-sp
- Author
- siriusaam
- Language
- EN