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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    Title :

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


    Contributors:

    Conference:

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


    Publication date :

    2017-06-05


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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