Incompressible

Find projects using the incompressible analysis type here. | Page 41

Optimization for a projectile used in a vacuum cannon for physics class.

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It has winglets, and an aerodynamic housing for the electronics.
Check holes 

Creation of a pinewood durby car model and testing aero and fluid principals using it

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Comparing CFD with actual measurements invivo

Complementação de dados barômetro caseiro

The leading edge is 5ft 6 inches
The last chord length (the one that connects the wingtip + wing) is 10.200 inches.
The offset is set to 6 inches back for the wingtip
The chord length of the the edge of the wingtip is 5.500 inches. - Copy

Courtesy of Jörn Beilke, joern@beilke-cfd.de , who supplied this file on the internet: http://www.beilke-cfd.de/Karmann_OpenFoam.tar.gz - Copy

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

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