In this part of the MEGADESIGN project, aeroelastic effects are introduced into the aerodynamic analysis of aircrafts by coupling DLR's flow solvers TAU and FLOWer to a Timoshenko-beam solver. The emerging aeroelastic solvers and a method for the automatic identification of Timoshenko-beam models for wing-box structures were integrated into a simulation environment enabling the combined optimisation of aerodynamic wing shape and structure.


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    Titel :

    Computational Methods for Aero-Structural Analysis and Optimisation of Aircrafts Based on Reduced-Order Structural Models


    Beteiligte:
    Reimer, L. (Autor:in) / Wellmer, G. (Autor:in) / Braun, C. (Autor:in) / Ballmann, J. (Autor:in)


    Erscheinungsdatum :

    2009


    Format / Umfang :

    16 Seiten





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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