Wing stiffness, mainly including bending stiffness and torsion stiffness, is very important in aircraft structure design. In order to research the relation between wing stiffness and optimization results, this paper makes optimization analysis to a composite T-tail configuration and a composite flying wing configuration based on different wing stiffness constraints, and some valuable conclusions are achieved.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Structural Optimization Research of Composite Aircraft Based on Different Wing Stiffness Constraints



    Erschienen in:

    Advanced Materials Research ; 466-467 ; 282-286


    Erscheinungsdatum :

    2012-02-10


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Aeroelastic Optimization of Variable Stiffness Composite Wing with Blending Constraints

    Bordogna, Marco Tito / Macquart, Terence / Bettebghor, Dimitri et al. | AIAA | 2016




    Aeroelastic Optimization of Variable Stiffness Composite Wing with Blending Constraints (AIAA 2016-4122)

    Bordogna, Marco Tito / Macquart, Terence / Bettebghor, Dimitri et al. | British Library Conference Proceedings | 2016