Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 with Area Suction Applied to Trailing-edge Flaps and with Several Wing Leading-edge Modifications


    Contributors:

    Publication date :

    1956-11-02


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English