A computational study on the aerodynamic properties of a pitching aerofoil with a morphing leading edge section at high Reynolds numbers

2026/06/20 by F. Madi, Y. Yao, M.P. O’Donnell +1

paper · doi:10.1016/j.ijheatfluidflow.2026.110531

published in International Journal of Heat and Fluid Flow 121, 110531 (Elsevier BV)

crossref created 2026/06/20 · crossref deposited 2026/08/05 · crossref indexed 2026/08/05 · crossref issued 2026/09/01 · crossref published 2026/09/01 · crossref published-print 2026/09/01

Citations

• Electroactive morphing effects on the aerodynamic performance through wobulation around an A320 wing with vibrating trailing edge at high Reynolds number
• Upstream Shear Layer Stabilisation via Self-Oscillating Trailing Edge Flaplets