The modal response of wing structures is very important for assessing their dynamic response including dynamic aeroelastic instabilities. Moreover, in a recent study an efficient structural optimization approach was developed using structural modes to represent the static aeroelastic wing response (both displacement and stress). In this paper, the modal response of general trapezoidal wing structures is approximated using shape sensitivities up to the 2nd order. Also different approaches of computing the derivatives are investigated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Modal Response of Trapezoidal Wing Structures Using Second Order Shape Sensitivities


    Beteiligte:
    Liu, Youhua (Autor:in) / Kapania, Rakesh K. (Autor:in)

    Erscheinungsdatum :

    01.01.2000


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch