Aerodynamic component and method for producing an aerodynamic component

摘要

An aerodynamic component (10) which in particular is suitable for use in an aircraft comprises an outer skin sheet (12) having an inner surface and an outer surface and being provided with a plurality of perforation openings (14) allowing a flow of air therethrough. The outer surface of the outer skin sheet (12) forms an aerodynamic surface of the aerodynamic component (10). The aerodynamic component (10) further comprises a sandwich panel (18) which includes an outer layer (20) facing the inner surface of the outer skin sheet (12), an inner layer (22) facing away from the inner surface of the outer skin sheet (12) and a foam core (24) sandwiched between the outer layer (20) and the inner layer (22). The sandwich panel (18) is provided with a plurality of connection openings (26) extending through the sandwich panel (18) between the outer layer (20) and the inner layer (22) and allowing a flow of air therethrough.