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1 Geometry
0 Meshes
0 Simulation setups
0 ResultsExternal incompressible CFD of a UAV fuselage (1.55 m) at 20 m/s. Cleaned watertight geometry. Outputs: drag coefficient, surface pressure, separation and wake vortices.
by slilbaekslilbaek
o_sanatuly created this project
about 1 month ago
1 Geometry 0 Meshes 0 Simulation setups 0 ResultsExternal incompressible CFD of a UAV fuselage (1.55 m) at 20 m/s. Cleaned watertight geometry. Outputs: drag coefficient, surface pressure, separation and wake vortices.
