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NACA 8-H-12 Airfoil Aerodynamics Study by Berat Akkaya is a document available to read on EtoBox.

What is NACA 8-H-12 Airfoil Aerodynamics Study about?

This document presents an investigation into the aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers ranging from 1.8 x 10^6 to 11.0 x 10^6. The study finds that the maximum lift coefficient of the NACA 8-H-12 is lower than that of commonly used airfoils, but it exhibits less sensitivity to leading-edge roughness. Overall, the NACA 8-H-12 airfoil demonstrates favorable aerodynamic properties, particularly in terms of drag coefficients at design lift conditions.

Author

Berat Akkaya

Language

EN