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Adaptive Aerodynamic Surface Control System for Supersonic Unmanned Aerial Vehicles

Patent #US11995610B2

Public record:Verify on Google Patents

A flight control mechanism that dynamically adjusts wing curvature to optimize lift-to-drag ratios at varying Mach speeds. The system improves fuel efficiency during high-altitude sustained flight.

Issue Date

5/5/2026

Inventor

David K. Nakamoto

Seller Location

United States

Price on request

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