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UCK305E NACA 64108 Airfoil CFD Study
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0 Geometries 0 Meshes 1 Simulation setup 0 ResultsAbout this project
This project investigates the aerodynamic performance of the NACA 64-108 airfoil using 2D CFD simulations. Lift, drag and pressure coefficient distributions are obtained at different angles of attack and compared with XFOIL results.
