The patent application relates to a device provided for attachment near the wing tip of an aircraft for the purpose of delivering a predetermined impulse to the wing for test purposes. Thrust is created by sudden release of fluid from a pressure vessel through one or more expulsion valves opening at an angle of approximately 90 degrees to the wing.


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    Titel :

    Wing Thruster


    Beteiligte:
    R. F. Vetter (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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