Compressible

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In this simulation, it is aimed to calculate the drag coefficient of an experimental rocket. Although the rocket geometry used is representative, the drag coefficient can be calculated for realistic models by following the simulation steps. K-w SST turbulence model was used for simulation. For the experimental rocket, the speed was taken 270 m / s and a ninety-degree (not realistic) flight angle assumption was made.

This is a simulation of the Hapsis 1 rocket nozzle

This is just a test to get simscale working.

flow analysis in wind tunnel using finite element methods

Obtención de CL max  para el ala de un UAV

Failed due to inconsistency in XYZT coordinates

Prova Simulazione flusso attraverso fori Ø3

Driver-Seegmiller supersonic validation casw