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1 Geometry
1 Mesh
1 Simulation setup
0 ResultsCFD investigation of a UAV wing with eagle-inspired winglets under crosswind conditions. The study evaluates aerodynamic forces, moments, pressure distribution, velocity distribution, and wingtip flow characteristics at different sideslip angles.
by slilbaekslilbaek
Kavitha24 created this project
9 days ago
1 Geometry 1 Mesh 1 Simulation setup 0 ResultsCFD investigation of a UAV wing with eagle-inspired winglets under crosswind conditions. The study evaluates aerodynamic forces, moments, pressure distribution, velocity distribution, and wingtip flow characteristics at different sideslip angles.
