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Dynamic Aerodynamic Airflow Control System for Supersonic Unmanned Aerial Vehicles

Patent #US12987002B1

Public record:Verify on Google Patents

A wing-integrated system using plasma actuators to manipulate boundary layer airflows at high speeds. The invention reduces drag and optimizes flight stability during transonic maneuvers.

Issue Date

5/5/2026

Inventor

Hiroshi Tanaka

Seller Location

United States

Price on request

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