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This conference paper presents a study on the effect of trailing edge serrations on the lift and drag characteristics of a NACA0012 airfoil wing, utilizing both computational and experimental methods. The research investigates two types of serrations—triangular and bird-type (quadratic spline)—to determine their impact on the lift-to-drag ratio at a constant Reynolds number of 360,000. The findings suggest that serrated edges can enhance aerodynamic performance by reducing drag and improving lift efficiency

Author

wick14244

Language

EN