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Panel - Compressible Flow in a Nozzle
Panel - Compressible Flow in a Nozzle(Tutorial Name) - Panel(Tutorial Name) - Panel

Compressible Flow in a Nozzle

Created using ANSYS 18.1

Problem Specification

Compute the converging-diverging nozzle flow using AIM and plot the pressure and velocity (Mach number) graphs. The pressure at the inlet is 3 bar at 300 K.


 

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