Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    High-speed Wind-tunnel Tests of an NACA 16-009 Airfoil Having a 32.9-percent-chord Flap with an Overhang 20.7 Percent of the Flap Chord


    Contributors:

    Publication date :

    1947-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English