This paper presents the results of an experimental and computational study of low-Reynolds number swept wing aerodynamics. This work has been conducted in preparation for icing effects on a swept wing. A complete abstract will be written for the final paper.


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    Titel :

    Low-Reynolds Number Aerodynamics of an 8.9 Percent Scale Semispan Swept Wing for Assessment of Icing Effects


    Beteiligte:
    Broeren, Andy (Autor:in) / Woodard, Brian (Autor:in) / Diebold, Jeff (Autor:in) / Moens, Frederic (Autor:in)

    Kongress:

    AIAA Atmospheric and Space Environments Conference 2017 ; 2017 ; Denver, CO, United States


    Erscheinungsdatum :

    05.06.2017


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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