Akademik Veri Yönetim Sistemi
AERONAUTICAL JOURNAL, 2025 (SCI-Expanded, Scopus)
The effect of the bio-inspired leading-edge modifications on the aerodynamic performance of non-slender delta wing models was investigated in a low-speed wind tunnel using force and surface pressure measurements. The measurements were performed at a Reynolds number of $Re = 1 \times {10<^>5}$ over an angle-of-attack range from $ - 4<^>\circ $ to $30<^>\circ $ . Seven different sharp-edged delta wing models with a 45-degree sweep angle ( ${\rm{\varLambda }}$ ), including a base wing, were used to study the effect of sinusoidal and saw-tooth leading-edge modifications. Sinusoidal leading-edge wing designs were inspired by the leading-edge tubercles of the humpback whale's pectoral fins. The results indicate that the bio-inspired wing modifications resulted in a delay in the stall angle by 4 degrees, smoother stall characteristics, a higher maximum lift coefficient, and increased post-stall lift. The drag coefficient of the modified wings was observed as higher than that of the base wing model. Regarding the longitudinal static stability, leading-edge modifications decreased the stability of the wing as the angle-of-attack surpassed $\alpha = 17<^>\circ $ .