Ten, natural-laminar-flow airfoils, the S406, S407, S409, S410, S411, S412, S413, S414, S415,and S418, intended for rotorcraft applications, have been designed and analyzed theoretically. Five of the airfoils, the S406, S407, S411, S414, and S415, have been experimentally verified. The measurements have been compared with predictions from two, widely used airfoil codes as well as from two, computational fluid dynamics codes.


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    Titel :

    Some New Airfoils for Rotorcraft


    Beteiligte:
    D. M. Somers (Autor:in)

    Erscheinungsdatum :

    2010


    Format / Umfang :

    37 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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