The disclosure relates to a wing 2 with at least two winglets 8,9,10 having a relative dihedral angle between them, and to an airplane 1 having such wings. An upstream winglet 8 broadens a region of inclined airflow, and a more downstream winglet 9 produces a thrust contribution therein.
AIRPLANE WING
FLUGZEUGFLÜGEL
AILE D'AVION
2021-12-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |