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    Detached-eddy simulations on massively separated flows over a 76/40° double-delta wing

    Detached-eddy simulations on massively separated flows over a 76/40° double-delta wing


    Abstract We investigated the flow past a 76/40° double-delta wing at angles of attack from 10° to 35° using SA-DES and a hybrid fourth-order scheme. Comparisons were made with the surface separation pattern, the pressure distribution and the location of vortex breakdown with experimental data, and acceptable agreement was obtained. Further discussions were made under the scenario of massively separated flows on topics such as the characteristics of conical flow, the structure of vortex breakdown and vortical substructures.

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    Titel :

    Detached-eddy simulations on massively separated flows over a 76/40° double-delta wing

    Beteiligte:
    Sun, Dong (Autor:in) / Li, Qin (Autor:in) / Zhang, Hanxin (Autor:in)
    Erschienen in:

    Aerospace Science and Technology ; 30 , 1 ; 33-45

    Erscheinungsdatum :

    2013-07-01

    Format / Umfang :

    13 pages

    ISSN :

    1270-9638

    DOI :

    https://doi.org/10.1016/j.ast.2013.07.001

    Medientyp :

    Aufsatz (Zeitschrift)

    Format :

    Elektronische Ressource

    Sprache :

    Englisch

    Schlagwörter :

    Detached-eddy simulation , Massively separated flows , Double-delta wing , Vortex breakdown , Vortex substructure

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