The present disclosure directed to an aircraft comprising one or more propulsion devices, a flexible wing, at least two tail booms having a proximal end and a distal end, the tail booms being secured to said flexible wing at the proximal end, wherein the tail booms comprise of a tail section connected at the distal end of said tail boom and wherein the tail section comprises of at least one control surface.
Wing-Twist Controlled Aircraft
2019-03-14
Patent
Elektronische Ressource
Englisch
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