The invention relates to a wing (2, 3) with two winglets (9-12) and a respective airplane. An upstream winglet broadens a region of inclined airflow and a downstream winglet produces a thrust contribution therein.
AIRPLANE WING
FLUGZEUGFLÜGEL
AILE D'AVION
2018-01-17
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |