Project

Simulating flow over NACA0017 airfoil with different angel of attacks

Objective: AIM: - Flow Simulation over NACA 0017 Airfoil. Objectives: - Model the flow over a NACA0017 airfoil For the angle of attacks 0,2,4,6,8,10 compare the lift and drag forces Formulas to calculate the dimensions of the airfoil: - NACA 4 digit airfoil specifications: This NACA airfoil series is controlled by 4 digits…

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