Self-adaptive high-speed aircraft layout based on wingtip deformation

The invention discloses a self-adaptive high-speed aircraft layout based on wingtip deformation. The self-adaptive high-speed aircraft layout comprises a center body, wings, two variable winglet and two one-way Flap rudders located at the rear ends of the lower surfaces of the wings. The center body...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GU XIANGYU, ZHAO JING, LOU YIZHI, LYU DIANJUN, LI TIANREN, CHEN PEIZHI, MA XIAOYUAN, MA MENGYING, SUN WEIXUAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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