Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Static Aeroelastic Analysis of Very Flexible Wing Based on the 3-D Lifting-Line Theory


    Beteiligte:
    Xie, Changchuan (Autor:in) / Liiu, Yi (Autor:in) / Yang, Chao (Autor:in)

    Kongress:

    53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference



    Erscheinungsdatum :

    01.01.2012




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Static Aeroelastic Analysis of Very Flexible Wing Based on the 3-D Lifting-Line Theory

    Xie, C. / Liu, Y. / Yang, C. et al. | British Library Conference Proceedings | 2012


    Aeroelastic Trim Analysis of Very Flexible Aircraft Based on 3-D Lifting-Line Theory

    Xie, C. / Liu, Y. / Yang, C. et al. | British Library Conference Proceedings | 2013



    Experimental Aeroelastic Benchmark of a Very Flexible Wing

    Avin, Or / Raveh, Daniella E. / Drachinsky, Ariel et al. | AIAA | 2022


    FINITE-STATE AEROELASTIC MODELLING OF MORPHING WING THROUGH UNSTEADY LIFTING-LINE THEORY

    Giansante, R. / Bernardini, G. / Gennaretti, M. | DataCite | 2024