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0 Geometries
0 Meshes
0 Simulation setups
0 ResultsNumerical investigation of the aerodynamic performance of a NACA 0012 airfoil at different angles of attack, focusing on lift, drag, and flow characteristics.
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by mwavinyamwavinya
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
oait_brik created this project
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsNumerical investigation of the aerodynamic performance of a NACA 0012 airfoil at different angles of attack, focusing on lift, drag, and flow characteristics.
