Yaw control surfaces were developed for a jet propelled aircraft. A thrust augmented rudder is disposed above the jet exhaust stream and a thrust rudder tab extends downward into the jet exhaust stream. These components are cooperatively deflected to generate yawing moments for directional control of the aircraft.


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    Titel :

    Thrust augmented spin recovery device


    Beteiligte:
    Berrier, B. L. (Autor:in)

    Erscheinungsdatum :

    1980-12-02


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    B. L. Berrier | NTIS | 1979


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