IbrahimBakry/Aerodynamic-Analysis-of-NACA-65A510-Airfoil-in-Compressor-Applications
This study performs a comprehensive CFD analysis of the NACA 65A510 airfoil profile, a widely used design in axial compressor blades, to evaluate its aerodynamic performance under varying angles of attack (α = 0°, 3°, 5°, 10°, 15°).
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