The present invention provides an aerodynamic structure (1), in particular for an aircraft (10), comprising a leading edge (2) having an outer structure, wherein the outer structure comprises: a first layer (3); and a second layer (4) geometrically corresponding to the first layer (3); wherein the first layer (3) is positioned on an outside (5) of the outer structure, the outside (5) being exposed to a flowing fluid, and the second layer (4) is positioned on an inside of the outer structure; and wherein the second layer (4) has a higher ductility than the first layer (3). Further the present invention provides an aircraft comprising such an aerodynamic structure.
AERODYNAMIC STRUCTURE AND AIRCRAFT
AERODYNAMISCHE STRUKTUR UND FLUGZEUG
STRUCTURE AÉRODYNAMIQUE ET AÉRONEF
2024-01-31
Patent
Electronic Resource
English
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