Results of investigation made in 7 × 10-ft wind tunnel on airfoil with several arrangements of venetian blind flaps to determine aerodynamic section characteristics as affected by overall flap chord, chords of slats used to form flap, slat spacing, number of slats, and position of flap with respect to wing.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Preliminary wind-tunnel investigation of N.A.C.A. 23012 airfoil with various arrangements of venetian-blind flaps


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


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


    Erscheinungsdatum :

    1940


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :