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)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    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





    Finite Element Analysis Validation for Stitched, Blade-Stiffened Aerospace Structures

    Anderson, Erin K. / Zahn, Alana / Lovejoy, Andrew E. | AIAA | 2022


    Finite Element Analysis Validation for Stitched, Blade-Stiffened Aerospace Structures

    Erin Anderson / Alana Zahn Cardona / Andrew E Lovejoy | NTRS


    Finite Element Analysis Validation for Stitched, Blade-Stiffened Aerospace Structures

    Erin Anderson / Alana Zahn Cardona / Andrew Lovejoy | NTRS


    Plotting Load Paths from Finite Element Stress Results for Aerospace Structures

    Kelly, Don / Pearce, Garth / Schroder-Turner, Khan | AIAA | 2019