Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Wind-Tunnel Tests of Ailerons at Various Speeds. 4 - Ailerons of 0.20 Airfoil Chord and True Contour with 0.35 Aileron-Chord Extreme Blunt-Nose Balance on the NACA 23012 Airfoil


    Contributors:

    Publication date :

    1943


    Size :

    48 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English