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Adaptive Aerodynamic Surface Control for Supersonic Commercial Aircraft Stability

Patent #US13452894B2

Public record:Verify on Google Patents

A morphing wing structure that automatically adjusts to varying air densities during the transition from subsonic to supersonic flight. The mechanism utilizes shape-memory alloys for frictionless surface contour modifications.

Issue Date

5/9/2026

Inventor

Sarah Jenkins

Seller Location

United States

Price on request

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