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
2015-07-14
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Variable-area canard forward-swept wing morphing aircraft
Europäisches Patentamt | 2020
|Wiley | 2020
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Online Contents | 1993