Reynolds-Averaged Navier-Stokes (RANS) computational fluid dynamics (CFD) analysis was conducted: to study the low-speed stall aerodynamics of a GIII aircrafts swept wing modified with (1) a laminar-flow wing glove, or (2) a seamless flap. The stall aerodynamics of these two different wing configurations were analyzed and compared with the unmodified baseline wing for low-speed flight. The Star-CCM+ polyhedral unstructured CFD code was first validated for wing stall predictions using the wing-body geometry from the First AIAA CFD High-Lift Prediction Workshop.


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    Title :

    Analysis of Low-Speed Stall Aerodynamics of a Business Jets Wing Using STAR-CCM+


    Contributors:
    T. Bui (author)

    Publication date :

    2016


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English