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In-compressible flow simulation for aerodynamic studies, using SimScale Standard mesh algorithm

Preliminary cfd analysis on the full sailplane

Endeavoring to become familiar with Hex parametric meshing

creation of the control volume mesh of a centrifugal pump

I am using this project to learn CFD on SimScale, how to perform convergence studies, and practice post-processing techniques. I have taught myself modeling using Onshape. I made a rear wing using Formula Student regulations and some averaged car dimensions. I have been modifying the design based on CFD results to learn how to manipulate airflow based on certain geometries.  I made sure to include as many of the scalars and vectors in the solution fields as to learn what each graph or image is telling me. I understand that designing a rear wing in free air is almost pointless due to how much the car's airflow changes the performance, so this is just used as a learning platform to get myself started.

This project has the goal to analyze the inlet airflow in a Formula SAE's airbox car. Particularly I want to simulate the velocity vectors and the pressure of the airflow to understand where to improve the airbox geometry. This will be achieved with a punctual reporting of mass flow outing from mesh, that represents the mass flow entrance in the cylinder of the engine. 
Final goal is to maximize the mass flow.

Check out www.simscale-academy.com for more classes on simulation.

To obtain a generic bolt fastener model meshing method.

The main aim of the project was trying to find stress and total displacement on the surface and check with experimental results. In this project, F1 halo is simulated in two different static load condition and for that use SIMULATION TYPE was STATIC. The halo is a driver crash protection system used in open wheel racing series which consists of a curved bar placed to protect the drivers head. The system was introduced in 2015 and became mandatory according to FIA homologation and regulation from 2018.

Simulation of lateral stability of a Thrush S-2R crop duster at high yaw and angle of attack. This airframe was originally designed for radial engines, so the addition of an extended nose to accommodate turbine power on these short-coupled, heavy-flying aircraft should be destabilizing. Let's find out how much! Extensive work (and detail!) on forming an appropriate mesh with adequate boundary layer.

Realisation of a plane using triangular elements

meshing | SimScale Project Library | Page 1