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Aerodynamic Analysis of NACA 0015 Airfoil by saadmuhammad3012 is a document available to read on EtoBox.
This project report investigates the aerodynamic behavior of a NACA 0015 airfoil through experimental and computational analysis under low-speed flow conditions. The study evaluates lift and drag coefficients at various velocities and angles of attack, utilizing both wind tunnel measurements and CFD simulations in ANSYS FLUENT. The results demonstrate the effectiveness of CFD techniques in analyzing airfoil aerodynamics, particularly in low Reynolds number regimes.
- Author
- saadmuhammad3012
- Language
- EN