Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on NACA 651-210 airfoil section. (Confidential Report L5F27 Dec 1945)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on NACA 651-210 airfoil section


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1945


    Size :

    19 pages


    Remarks:

    37 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :