A novel solution methodology for longitudinal flight characterization of a Flying-Wing Micro Aerial Vehicle
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DOI: 10.1177/09544100221081845
Abstract: A longitudinal flight dynamic study of a low mass moment of inertia vehicle is presented. Aerodynamic and stability derivatives of a flying-wing microaerial vehicle (FWMAV) were obtained through detailed subsonic wind tunnel tests at a… read more here.
Keywords: methodology; velocity; flying wing; longitudinal flight ... See more keywords