The invention relates to an aircraft having at least one wing (5) including, at each end thereof, a fin (6) forming an angle of between 0° and 45° relative to the vertical. According to the invention, each fin (6) has a leading edge (7) that includes at least one slot (8) provided along said leading edge (7) and oriented so as to cause an air flow to flow via said leading edge (7) from an outer surface (6a) of the fin (6) to an inner surface (6b).
AERONEF A VOILURE FIXE ET A STABILITE STATIQUE ACCRUE
2018-07-20
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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