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1 Geometry
1 Mesh
1 Simulation setup
0 ResultsSeveral custom airfoil cross-sections will be designed and tested under identical flow conditions. For each profile, the lift force, drag force, pressure distribution, and aerodynamic coefficients will be evaluated. The results will then be compared to determine which geometric characteristics lead to higher lift, lower drag, and a better lift-to-drag ratio. The simulations will also serve as a basis for comparison with experimental measurements performed in a self-built wind tunnel. The overall objective is to investigate the relationship between airfoil geometry and aerodynamic performance and to determine whether the CFD results correspond to the experimental data.
therealdodo created this project
30 days ago
1 Geometry 1 Mesh 1 Simulation setup 0 ResultsSeveral custom airfoil cross-sections will be designed and tested under identical flow conditions. For each profile, the lift force, drag force, pressure distribution, and aerodynamic coefficients will be evaluated. The results will then be compared to determine which geometric characteristics lead to higher lift, lower drag, and a better lift-to-drag ratio. The simulations will also serve as a basis for comparison with experimental measurements performed in a self-built wind tunnel. The overall objective is to investigate the relationship between airfoil geometry and aerodynamic performance and to determine whether the CFD results correspond to the experimental data.
by slilbaekslilbaek
