Set up your own cloud-native simulation in minutes.Start Simulating Now
0
0
1 Geometry
3 Meshes
2 Simulation setups
2 ResultsExternal aerodynamic CFD of the repaired NACA 4412 wing and right endplate/support. Baseline assumptions: air at 25 C, incompressible steady flow, 15 m/s inlet; evaluate drag, lift/downforce and lift-to-drag ratio.
december_olive created this project
22 days ago
1 Geometry 3 Meshes 2 Simulation setups 2 ResultsExternal aerodynamic CFD of the repaired NACA 4412 wing and right endplate/support. Baseline assumptions: air at 25 C, incompressible steady flow, 15 m/s inlet; evaluate drag, lift/downforce and lift-to-drag ratio.
