The invention relates to an aerodynamic device (1, 11), in particular an aerodynamic device for an aircraft comprising a frame (2), a skin (6) forming an aerodynamic surface and connected to the frame (2) and comprising a motile portion (4) adapted to be displaced between a first position in which the aerodynamic surface exhibits a first shape, and a second position different from the first position, characterized in that it comprises a disturbing structure (3), and in the second position of the motile portion (4), the aerodynamic surface exhibits a second shape in which the disturbing structure (3) induces a protrusion (14) on the aerodynamic surface.
AERODYNAMICS INFLUENCING DEVICE FOR AN AIRCRAFT AND AIRCRAFT
VORRICHTUNG ZUR BEEINFLUSSUNG DER AERODYNAMIK FÜR EIN FLUGZEUG UND FLUGZEUG
DISPOSITIF INFLUENÇANT L'AÉRODYNAMIQUE POUR AÉRONEF ET AÉRONEF
2019-10-16
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AERODYNAMICS INFLUENCING DEVICE FOR AN AIRCRAFT AND AIRCRAFT
European Patent Office | 2019
|TIBKAT | 1978
|Aircraft computational aerodynamics
British Library Conference Proceedings | 1998
|Aircraft computational aerodynamics
British Library Conference Proceedings | 1994
|Aircraft computational aerodynamics
British Library Conference Proceedings | 1996
|