Simulation of Flow over NACA AirFoil in SolidWorks
Objective: RESULTS Obtained: (A) Angle of Attack = 0 Degree: (B) Angle of Attack = 2 Degree: (C) Angle of Attack = 4 Degree: (D) Angle of Attack = 6 Degree: (E) Angle of Attack = 8 Degree: (F) Angle of Attack = 10 Degree: Lift…