RANS modelling of some strongly swirling aerospace flows

    Research output: Contribution to journalArticlepeer-review

    Abstract

    Progress is reported on the modelling, via RANS closures, of two swirling turbulent flows important in aeronautics: the trailing wing-tip vortex and the flow in rotor-stator cavities. For the former the decay of the vortex is only well captured at second-moment level while, for the latter, an unsteady flow computation brings out large-scale organized structures, with the number of structures varying with cavity aspect ratio and Reynolds number, a result qualitatively in accord with experiment. © 2009 AFM EDP Sciences.
    Original languageEnglish
    Pages (from-to)171-174
    Number of pages3
    JournalMecanique et Industries
    Volume10
    Issue number3-4
    DOIs
    Publication statusPublished - May 2009

    Keywords

    • Fluids dynamics unsteady flows
    • Large-scale organized structures
    • Modelling
    • RANS

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