The calculations described were carried out for an F28-Mk 1000 C aircraft with a large cargo door. Using the ASKA program system, based on the finite element method, a great part of the fuselage, embedding the wingbox connection and the adjacent cargo door, was divided into about 3000 elements of different types: membrane and beam elements. Two loading cases, a cabine pressure case, and a fuselage bending case were considered. Results of calculations are compared with results of measurements on the structure.


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    Title :

    Calculation of Strength and Stiffness of an Aeroplane Fuselage Part with a Large Cargo Door


    Contributors:
    C. J. Lof (author) / H. H. Ottens (author)

    Publication date :

    1976


    Size :

    73 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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