A forebody flow control system and more particularly an aircraft or missile flow control system for enhanced maneuverability and stabilization utilizes various types of sensors and various types of activatable flow effectors to maneuver the aircraft or missile with the help of a control system. A method of operating the flow control system is also disclosed.
Flow control device and method for aircraft and missile forebody
30.08.2016
Patent
Elektronische Ressource
Englisch
Aircraft and missile forebody flow control device and method of controlling flow
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