SimScale simulation projects by salmghlab58 | Page 1

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simulate to gas disepertions from chimney

calculate lift coefficient and drag coefficient at variable AOA

calculate of lift ,drag and moment coefficient of wing and distribution of pressure and velocity in x direction

This tutorial aims to showcase how to set up a compressible analysis. An aircraft wing geometry is used.

This project aims to showcase the process of setting up and running an incompressible analysis. As a geometry, we have a Francis turbine. A MRF Rotating Zone is used for the runner.

Tutorial project for a stress analysis of a connecting rod. The project only provides the geometry to start with. See our tutorials section to have a look at the step-by-step instructions to set up the simulation.

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