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Converging Diverging Rocket Nozzle (Request 2 redux)

Converging Diverging Rocket Nozzle (Request 2 redux)

grabcad

The CD rocket nozzle has been redesigned using SolidWorks and exported as STL files for CFD software usage. The nozzle features an Ae/A* ratio of 14.06 and Ai/A* of 1.602, while STL surfaces of the inlet and outlet are also provided for CFD simulations. This redesign was previously posted on Rocket Nozzle request 2.

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