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This project  involves meshing a single-Shaft Turbofan Engine, and then simulating its' operation when facing an axial airflow of 150 m/s, while rotating with a velocity of 940 rad/sec (9000 rpm) . A Fan is used to bypass a large amount of air in the inside of the engine. For this case the typical Compressor, Combustion chamber and Turbine Stator were omitted, and only the Fan, Shaft, Shell and Turbine rotor were meshed and examined, in order to restrain the meshing requirements for complex, time consuming meshing and simulation.  A steady state incompressible flow simulation is executed to visualize the air flow through the components of the Turbofan, as well as the pressure and U magnitude distribution on the blades of the Fan and Turbine.

Link to  the extended compressible study (bigger domain included) : https://www.simscale.com/projects/fsite/turbofan_engine_extended_study/ - Copy - Copy

Simulation of various parameters arounds an ariplane wing

Testing Wing flow to make sure it's correct.

Drone propeller flow analysis simulation using MRF model and SimScale standard mesher. - Copy - Copy

1st Simulation of a data centre corridor to get a sense of how this app/website works

ES un proyecto de F1 in schools en donde ese va a evaluar el alerón

Public Projects