1. Numerical and experimental investigation of aspect ratio effect on aerodynamic performance of NACA 4415 airfoil section at low reynolds number
Hatice Cansu Ümütlü Ayaz, Zeki Kıral, Ziya Haktan Karadeniz, 2025, izvirni znanstveni članek

Ključne besede: airfoil, wind tunnel, aspect ratio effect, aerodynamic coefficients, three-component balance, low Reynolds number
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