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RANS modelling of some strongly swirling aerospace flows
Published online by Cambridge University Press: 05 August 2009
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.
Keywords
- Type
- Research Article
- Information
- Mechanics & Industry , Volume 10 , Issue 3-4: 19e Congrès français de mécanique (CFM 2009) , May 2009 , pp. 171 - 174
- Copyright
- © AFM, EDP Sciences, 2009