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This project analyzes wing aerodynamics using SimScale CFD. A FreeCAD-designed wing is tested in incompressible flow with the k-ω SST turbulence model. Simulations at −5° to 15° AoA provide lift (CL) and drag (CD) data. Results include lift curves, drag polars, and flow visualizations for aerodynamic performance evaluation.
by slilbaekslilbaek
Kavitha24 created this project
3 months ago