Evaluating the effect of a leading-edge slat on the aerodynamics of the NACA0018 airfoil

CC BY-ND 4.0Theron, Johannes NicolaasJohannes NicolaasTheronKassem, HassanHassanKassemManelil, Neeraj PaulNeeraj PaulManelilHöning, LeoLeoHöning2024-12-042024-12-042024-11-14https://doi.org/10.24406/publica-3879https://publica.fraunhofer.de/handle/publica/47962410.24406/publica-3879en600 Technik, Medizin, angewandte WissenschaftenEvaluating the effect of a leading-edge slat on the aerodynamics of the NACA0018 airfoilpresentation