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1 Geometry
2 Meshes
1 Simulation setup
4 ResultsComputational investigation of a NACA 4412 UAV wing with bio-inspired winglets under crosswind conditions. The study focuses on aerodynamic forces, moments, pressure distribution, velocity flow, wingtip vortices, and lateral aerodynamic characteristics during different sideslip angles.
by slilbaekslilbaek
Kavitha24 created this project
10 days ago
1 Geometry 2 Meshes 1 Simulation setup 4 ResultsComputational investigation of a NACA 4412 UAV wing with bio-inspired winglets under crosswind conditions. The study focuses on aerodynamic forces, moments, pressure distribution, velocity flow, wingtip vortices, and lateral aerodynamic characteristics during different sideslip angles.
