Set up your own cloud-native simulation in minutes.Start Simulating Now
1
0
2 Geometries
2 Meshes
5 Simulation setups
7 ResultsCFD analysis of NACA 2412 tapered wing to determine lift, drag and pressure distribution at various angles of attack. Part of aerospace engineering portfolio.
by slilbaekslilbaek
srikruti created this project
4 months ago
2 Geometries 2 Meshes 5 Simulation setups 7 ResultsCFD analysis of NACA 2412 tapered wing to determine lift, drag and pressure distribution at various angles of attack. Part of aerospace engineering portfolio.
