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This paper presents an analysis and optimization of aerofoil profiles, focusing on a standard symmetrical NACA 0012 aerofoil. Through Computational Fluid Dynamics (CFD), eight modified aerofoil shapes were created by altering chord thickness while maintaining maximum thickness. The study evaluates aerodynamic characteristics, including lift and drag coefficients, to identify the best-performing aerofoil for applications in compressors and turbines.

Author

mithij158

Language

EN