Calculation results are presented for the interference of a flat sweptback wing and a cylindrical fuselage at transonic speeds and small angles of attack. A random law of spanwise load distribution is used. Results are graphically presented and compared with experimental data. (Author)


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    Title :

    Interference of a Sweptback Wing and the Fuselage at Transonic Speeds


    Contributors:

    Publication date :

    1974


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English