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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    Title :

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


    Contributors:
    Reimer, L. (author) / Wellmer, G. (author) / Braun, C. (author) / Ballmann, J. (author)


    Publication date :

    2009


    Size :

    16 Seiten





    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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