Tests indicated that increasing aileron profile thickness from that of true contour to that of straight sided aileron would increase positively rate of change of aileron section hinge moment coefficient with both section angle of attack and aileron deflection, and would cause little change in hinge moment parameter for given rate of roll at low aileron deflections.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Investigation of approximately 0.178-chord-thick NACA 6-series-type airfoil section equipped with sealed internally balanced 0.20-chord ailerons and with 0.05-chord tab


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Visconti, F. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :