The report documents a study made of the optimization of typical aircraft structural components using the Automated Structural Optimization Program (ASOP) described in AFFDL-TR-70-118. The structures examined were a fuselage structure for a proposed space shuttle orbiter and a wing structure for the same vehicle. Examples are given of practical finite element modeling of these structures. (Author)


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    Titel :

    Finite Element Modeling and Optimization of Aerospace Structures


    Beteiligte:
    W. J. Dwyer (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    58 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch