Some numerical aspects for the coupling process of a discrete non-linear aeroelastic system are presented. The objective of this paper is two-fold: first, a consistent time-integration method of the whole coupled system is developed and the robustness is shown. Second, several data transfer methods — conservative interpolation, Galerkin-based transfer, dual-Lagrange-based transfer, and Sobolev-norm-based transfer — are employed and the importance of an accurate transfer scheme is demonstrated. Numerical results obtained from simulations of an oscillating one-dimensional plate in a transonic flow and a three-dimensional wing example serve as a typical benchmark problem to show the applicability of the presented concepts and the importance on the behaviour of an aeroelastic system.


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    Title :

    Coupling techniques for computational non-linear transient aeroelasticity


    Contributors:
    Unger, R (author) / Haupt, M C (author) / Horst, P (author)


    Publication date :

    2008-04-01


    Size :

    13 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Coupling techniques for computational non-linear transient aeroelasticity

    Unger, R. / Haupt, M.C. / Horst, P. | Tema Archive | 2008


    Coupling techniques for computational nonlinear transient aeroelasticity

    Unger, Ralf / Haupt, Matthias C. / Horst, Peter | Tema Archive | 2006


    Computational Linear Aeroelasticity and Aeroservoelasticity

    Gupta, Kajal K. / Meek, John L. | AIAA | 2003