Aerodynamic force tests conducted in vertical wind tunnel; increase of 41.5 per cent in max. lift; angle of attack for max. lift increased 13 deg.; max. increase of 30 deg. possible in highest stalling angle.


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    Titel :

    Aerodynamic characteristics of slotted clark Y wing as affected by auxiliary airfoil position


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics -- Report


    Beteiligte:
    Wenzinger, C.J. (Autor:in) / Shortal, J.A. (Autor:in)


    Erscheinungsdatum :

    1931


    Format / Umfang :

    16 pages


    Anmerkungen:

    31 Figs.


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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