A mathematical model for crash simulation of aircraft structures--built up from beams, stringers, and skin panels--is being developed in the form of a finite element, large displacement elastic-plastic computer code called DYCAST. As a preliminary exercise, the code was applied to simulate a low-speed forward impact of a skin-covered framework carrying large concentrations of nonstructural mass at its rear. This paper describes the main features of the code and the results of the simple preliminary simulation.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Crash Simulation of Skin-Frame Structures using a Finite Element Code


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Pifko, Allan B. (Autor:in) / Armen, Harry (Autor:in) / Winter, Robert (Autor:in)

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1977



    Erscheinungsdatum :

    01.02.1977




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Front Crash Analysis of a Steel Frame Auto Using a Finite Element Computer Code

    Winter,R. / Crouzet-Pascal,J. / Pifko,A.B. et al. | Kraftfahrwesen | 1984


    Front Crash Analysis of a Steel Frame Auto Using a Finite Element Computer Code

    Pifko, Allan B. / Crouzet-Pascal, Jacques / Winter, Robert | SAE Technical Papers | 1984


    Finite element modelling of metallic tubular crash structures with an explicit code

    Silcock, M. / Hall, W. / Fox, B. et al. | Tema Archiv | 2006


    Finite Element Modeling of Composite Tubular Crash Structures With an Explicit Code

    Fox, B. / Society of Automotive Engineers | British Library Conference Proceedings | 2006


    Finite element modelling of metallic tubular crash structures with an explicit code

    Silcock,M. / Hall,W. / Fox,B. et al. | Kraftfahrwesen | 2006