Aerodynamics Part 3: Control Surfaces & Tapered Aileron Geometry
2026-07-27

Aerodynamics Part 3: Control Surfaces & Tapered Aileron Geometry

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A sharp tapered aileron geometry narrowing from 104 mm at the root to 46 mm at the wingtip was engineered. Reaching a 44% chord ratio at the wingtip provides immediate roll authority during tight search turns. The tapered area distribution reduces aerodynamic hinge torque load to 3.3 kg . cm, preventing servo overload.