Set up your own cloud-native simulation in minutes.Start Simulating Now
NACA 0012 Airfoil CFD Analysis (H.B) - Copy
0
0
Statistics
1 Geometry
3 Meshes
2 Simulation setups
2 Results
1 Geometry 3 Meshes 2 Simulation setups 2 ResultsAbout this project
In 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
