Aerospace vehicle structures must be optimized for mass to maximize the mission payload. During the conceptual design phase, structures must be optimized to accurately predict the mass of the design. Analysis methods that are used in sizing members should allow for the selection of a variety of metallic and composite materials and user-defined geometry constraints. Rapid vehicle structural analysis is often necessary to improve the fidelity and the results that are obtained during the preliminary design. Recent experiences are highlighted that utilize the Collier Research Corporation's Hypersizer toolset to optimize structural concepts.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Structural Optimization of Conceptual Aerospace Vehicles


    Beteiligte:

    Kongress:

    HPSM 2008: 4th International Conference on High Performance Structures and Materials ; 2008 ; The Algarve, Portugal


    Erscheinungsdatum :

    2008-05-13


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Structural optimization of conceptual aerospace vehicles

    Hrinda, G.A. | British Library Conference Proceedings | 2008


    Structural bonding needs for aerospace vehicles

    Reinhart, T.J. | Tema Archiv | 1989


    Structural bonding needs for aerospace vehicles

    Reinhart, T.J. | Tema Archiv | 1989