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Supersonic Nozzle

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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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Project History

  • quetglas_morera

    quetglas_morera created this project

  • 15_10833

    15_10833 copied this project