An aircraft includes a fuselage, a main wing pivotally coupled to an aft portion of the fuselage, and a canard coupled to a forward portion of fuselage, wherein the main wing and the canard are configured to be connected together for supersonic flight and disconnected from each other for subsonic flight.
CANARD-LOCKED OBLIQUE WING AIRCRAFT
ENTENFLUGZEUG MIT DREHENDER TRAGFLÄCHE
AVION À AILE OBLIQUE À BLOCAGE DE CANARD
2017-01-04
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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