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Adaptive Aerodynamic Flow Control System for Supersonic Aerospace Vehicle Surfaces

Patent #US11995877B2

Public record:Verify on Google Patents

A synthetic jet actuator system embedded into the skin of aerospace vehicles to manipulate boundary layer airflow. This system actively reduces drag and optimizes flight stability during transonic and supersonic transitions.

Issue Date

5/10/2026

Inventor

Arthur P. Vance

Seller Location

United States

Price on request

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