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.


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    Titel :

    Flow control device and method for aircraft and missile forebody


    Beteiligte:
    SOWLE ZAK (Autor:in) / VASUDEVAN SRIKANTH (Autor:in) / STUCKE RUSSELL (Autor:in) / LISY FREDERICK J (Autor:in) / SCHMIDT ROBERT N (Autor:in)

    Erscheinungsdatum :

    30.08.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen / B64C AEROPLANES , Flugzeuge



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