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Modular Aerodynamic Winglets with Shape-Memory Alloy Actuation for Supersonic Flight

Patent #US13994566B2

Public record:Verify on Google Patents

Variable geometry wing structures that adjust in real-time based on atmospheric pressure and velocity. This reduces drag coefficients during transition phases into supersonic flight regimes.

Issue Date

5/5/2026

Inventor

Katherine Vance

Seller Location

United States

Price on request

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