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1 Geometry
3 Meshes
2 Simulation setups
2 ResultsIn this project we examined the Effect of Boundary Layers on the NACA 0012 Airfoil. In-compressible fluid flow simulation is selected for the project. Free stream velocity is selected as 10 m/s having A.O.A 10 with the airfoil. - Copy
by simscalesimscale
1 Geometry 3 Meshes 2 Simulation setups 2 ResultsIn this project we examined the Effect of Boundary Layers on the NACA 0012 Airfoil. In-compressible fluid flow simulation is selected for the project. Free stream velocity is selected as 10 m/s having A.O.A 10 with the airfoil. - Copy
HamzaBaig created this project
over 7 years ago
shi42 copied this project
6 months ago
