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:
    A. Broeren (Autor:in) / B. Woodard (Autor:in) / J. Diebold (Autor:in) / F. Moens (Autor:in)

    Erscheinungsdatum :

    2017


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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