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    Titel :

    Aeroestructural Design Optimization of a Subsonic Wing with Continuous Morphing Trailing Edge


    Beteiligte:

    Kongress:

    35th AIAA Applied Aerodynamics Conference



    Erscheinungsdatum :

    01.01.2017




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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