Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic characteristics of a wing with quarter chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section transonic-bump method


    Contributors:

    Publication date :

    1949-07-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English