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0 Geometries
0 Meshes
0 Simulation setups
0 ResultsExternal incompressible CFD of a 4 m span quad-plane VTOL at 20 m/s. Wing AR 12, NACA 4412-4410, V-tail. Outputs: drag and lift coefficients, L/D, surface pressure, wake vortices.
by slilbaekslilbaek
o_sanatuly created this project
about 1 month ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsExternal incompressible CFD of a 4 m span quad-plane VTOL at 20 m/s. Wing AR 12, NACA 4412-4410, V-tail. Outputs: drag and lift coefficients, L/D, surface pressure, wake vortices.
