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External aerodynamics of a lift+cruise VTOL fixed-wing UAV. Span 3.99 m, fuselage length 1.88 m. Geometry exported from Fusion as merged outer skin (STEP, mm). Symmetry plane at Z = -165 mm.
by slilbaekslilbaek
olzas574 created this project
15 days ago
External aerodynamics of a lift+cruise VTOL fixed-wing UAV. Span 3.99 m, fuselage length 1.88 m. Geometry exported from Fusion as merged outer skin (STEP, mm). Symmetry plane at Z = -165 mm.