Wind-tunnel tests of rectangular Clark Y wing made with N A C A spinning balance; all six components of aerodynamic force and moment were measured throughout range of angles of attack and angles of sideslip, likely to be attained by spinning airplane; application of data from spinning balance to estimation of angle of sideslip necessary for spinning equilibrium at any angle of attack. (Price 10¢)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Spinning characteristics of wings. I -- Rectangular Clark Y monoplane wing


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Bamber, M.J. (Autor:in) / Zimmerman, C.H. (Autor:in)


    Erscheinungsdatum :

    1935


    Format / Umfang :

    20 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :