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4 Geometries
7 Meshes
3 Simulation setups
3 ResultsThis project investigates the aerodynamic behaviour of a finite-span NACA 0012 wing using 3D CFD in SimScale. The wing has a 100 mm chord and 200 mm span and will be analysed at different angles of attack, initially 0°, 5°, and 10°. The objective is to study lift, drag, aerodynamic efficiency, pressure distribution, wake development, and finite-span effects such as wingtip vortices. The results will later support the development of a simplified Formula 1 rear-wing model and comparison with experimental wind-tunnel testing.
nhajee created this project
14 days ago
4 Geometries 7 Meshes 3 Simulation setups 3 ResultsThis project investigates the aerodynamic behaviour of a finite-span NACA 0012 wing using 3D CFD in SimScale. The wing has a 100 mm chord and 200 mm span and will be analysed at different angles of attack, initially 0°, 5°, and 10°. The objective is to study lift, drag, aerodynamic efficiency, pressure distribution, wake development, and finite-span effects such as wingtip vortices. The results will later support the development of a simplified Formula 1 rear-wing model and comparison with experimental wind-tunnel testing.
