Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Chordwise pressure distribution at high subsonic speeds near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil sections and equipped with various spoiler ailerons


    Contributors:

    Publication date :

    1952-06-24


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English