Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Lateral-control investigation of flap-type controls on a wing with quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bump method


    Contributors:

    Publication date :

    1950-01-25


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English