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    Titel :

    Computational Investigation of the Effect of Sweep on a Pitching Finite-Aspect-Ratio Wing


    Beteiligte:

    Kongress:

    2018 AIAA Aerospace Sciences Meeting



    Erscheinungsdatum :

    01.01.2018




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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