The present paper deals with steady and unsteady aeroelastic simulation results obtained on the High Reynolds Number Aero-Structural Dynamics (HIRENASD) wind tunnel configuration [1], selected as common test case in the numerical aeroelasticity ONERA/DLR cooperation project “NLAS2”. In order to assess the aeroelastic prediction capabilities of the flow solvers elsA (ONERA) and TAU (DLR), 3 types of simulations have been realized: static coupling, harmonic forced motion and dynamic coupling. The set-up of the numerical simulations as well as comparisons with experimental data are presented for selected test cases.


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    Title :

    Assessment of the ONERA/DLR numerical aeroelastics prediction capabilities on the HIRENASD configuration


    Contributors:
    Hassan, D. (author) / Ritter, Markus (author)

    Conference:

    2011 ; Paris, Frankreich



    Publication date :

    2011


    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    German




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