Compressive load capacity of composite lattice structures are studied. The objective of this research is to investigate the buckling strength of composite lattice structures and to design the most weight efficient structure with the highest buckling load. Buckling strength of both the composite lattice cylindrical and conical shells under axial compressive loads are examined. The main emphasis is placed on the effects of geometric constraints and the optimal design of the structures.In this research, various constraints are studied and the optimal structure which gives the highest strength to weight ratio is obtained. Moreover, these structures can be constructed by filament winding, the manufacturing process can be automated, and the costs can be greatly reduced.


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    Titel :

    Design and Fabrication of Composite Attach Fitting for Satellite Launch Vehicle


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Hou, An (Autor:in) / Gramoll, Kurt (Autor:in)

    Kongress:

    Aerospace Manufacturing Technology Conference & Exposition ; 1998



    Erscheinungsdatum :

    1998-06-02




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Design and Fabrication of Composite Attach Fitting for Satellite Launch Vehicle

    Hou, A. / Gramoll, K. / Society of Automotive Engineers | British Library Conference Proceedings | 1998


    Compressive Strength of Composite Attach Fitting for Launch Vehicle

    Hou, A. / Gramoll, K. / Canadian Society for Mechanical Engineering | British Library Conference Proceedings | 1998




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