A wing (3) comprising at least one aerofoil section and having a leading edge (5), a trailing edge (6), an upper surface and a lower surface (8), wherein a region within the aerofoil section immediately adjacent the leading edge (5) is ventilated so as to establish a sub-static pressure in that region during flight. Also, a method of operating the wing.
Wing leading edge venting
Flügelvorderkantendurchlüftung
Ventilation de bord d'attaque d'une aile
2018-12-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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