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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.
![](/download/attachments/348591726/image2017-8-7%2012%3A29%3A8.png?version=1&modificationDate=1502123369000&api=v2)
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