In this paper a new fast preliminary design analysis tool is presented for identifying structural concept models of composite wing structures with emphasize on bend-twist coupling. The research focused on the analysis of a box-beam load carrying structure of a wing using an in-house code. Results are compared and validated with analytical, numerical and experimental data available in published literature. The developed tool is used to evaluate the aeroelastic response of the load bearing structure of a composite wing. A fast qualitative analysis of the wing box response is made based on the predicted bend and twist behavior proving the usefulness of such preliminary design tools.


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    Titel :

    Aeroelastic tailoring of thin-walled, closed-section wing box with bend-twist coupling


    Beteiligte:


    Erscheinungsdatum :

    01.07.2017


    Format / Umfang :

    401679 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Some Basic Strategies for Aeroelastic Tailoring of Wings with Bend-Twist Coupling: Part One

    Rehfield, L. / Cheung, R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003




    Strategies for Tailoring Wings with Bend-Twist Coupling: Part Two

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    Aeroelastic Tailoring of Metallic Wing Structures

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