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2 Geometries
5 Meshes
1 Simulation setup
2 ResultsExternal incompressible CFD of a UAV fuselage (1545 x 274 x 330 mm) to obtain drag and lift coefficients and surface pressure distribution.
by slilbaekslilbaek
olzas574 created this project
15 days ago
2 Geometries 5 Meshes 1 Simulation setup 2 ResultsExternal incompressible CFD of a UAV fuselage (1545 x 274 x 330 mm) to obtain drag and lift coefficients and surface pressure distribution.
