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0 Results2D CFD simulation of NACA 4412 airfoil. To study the effect of angle of attack (0° to 25°) on lift coefficient, drag coefficient and lift-to-drag ratio. Incompressible steady-state simulation with k-omega SST turbulence model, for race car rear wing aerodynamic design reference.
by mwavinyamwavinya
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
JudeXu1 created this project
18 days ago
0 Geometries 0 Meshes 0 Simulation setups 0 Results2D CFD simulation of NACA 4412 airfoil. To study the effect of angle of attack (0° to 25°) on lift coefficient, drag coefficient and lift-to-drag ratio. Incompressible steady-state simulation with k-omega SST turbulence model, for race car rear wing aerodynamic design reference.
