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Aerodynamic Variable Geometry Airfoil For Hypersonic Flight Maneuverability Enhancement

Patent #US12944505B2

Public record:Verify on Google Patents

An integrated control system for adjustable trailing edge surfaces on hypersonic aircraft. It provides real-time thermal expansion compensation to maintain aerodynamic efficiency at speeds exceeding Mach 5.

Issue Date

5/5/2026

Inventor

Robert A. Sinclair

Seller Location

United States

Price on request

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