Methods, apparatus, and articles of manufacture to extend a leading-edge vortex of a highly-swept wing aircraft wing are disclosed. An example apparatus includes a shoulder wing coupled to a fuselage of an aircraft above a highly-swept wing of the aircraft, the shoulder wing operative in a first position to extend a leading-edge vortex spanwise along the highly-swept wing of the aircraft.
METHODS AND APPARATUS TO EXTEND A LEADING-EDGE VORTEX OF A HIGHLY-SWEPT AIRCRAFT WING
2018-06-21
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Methods and apparatus to extend a leading-edge vortex of a highly-swept aircraft wing
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