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Nozzle exit flow visualization
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1 Geometry
1 Mesh
1 Simulation setup
2 Results
1 Geometry 1 Mesh 1 Simulation setup 2 ResultsAbout this project
To visualize and analyze the flow pattern at the exit of a converging-diverging (C-D) nozzle, including: Shock waves Expansion fans Mach disk formation (in supersonic flow) Effect of back pressure This helps understand real nozzle flow behavior, which is directly relevant to rocket propulsion.
