An airfoil for a rotor blade of a rotary wing aircraft, the airfoil having a predetermined maximum thickness to chord ratio and comprising, between a leading edge and a trailing edge, an extrados and an intrados, the intrados being defined by predetermined intrados coordinate value pairs and the extrados being defined by predetermined extrados coordinate value pairs, wherein a maximum error of each one of the predetermined intrados coordinate value pairs and the predetermined extrados coordinate value pairs amounts to ±3%.


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    Titel :

    AIRFOILS FOR ROTOR BLADES OF ROTARY WING AIRCRAFTS


    Beteiligte:
    KLEIN ALEXANDER (Autor:in) / ILLG JONAS (Autor:in) / LUTZ THORSTEN (Autor:in) / ROHARDT CLAAS-HINRIK (Autor:in) / RICHTER KAI (Autor:in)

    Erscheinungsdatum :

    2017-01-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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