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    Title :

    Experiments on a 20 per cent. control with tab, fitted to NACA 0015 aerofoil, with especial reference to effect of its section on hinge moment and lift




    Publication date :

    1949


    Size :

    27 S.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik