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Supersonic Nozzle
403 4
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7 Geometries 6 Meshes 3 Simulation setups 11 Results
About this project
A convergent-divergent nozzle studied at 7MPa and 2558K of total pressure and temperature in the inlet and 101.5KPa and 263.15K at the outlet
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by Ali_ArafatAli_Arafat
Project History
quetglas_morera created this project
15_10833 copied this project