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Generation of a turbulent boundary layer inflow for RANS simulations
conference contribution
posted on 2016-02-24, 11:32 authored by Aldo Rona, M. Grottadaurea, M. Monti, C. Airiau, T. GandhiThe generation of a fully turbulent boundary layer profile is investigated using analytical and numerical methods over the Reynolds number range 300 ≤ Reθ ≤ 31000. The predictions are validated against reference wind tunnel measurements under zero streamwise pressure gradient. The analytical method is then tested for favourable pressure gradient by modelling the turbulent boundary layer approaching a two-dimensional potential sink. Both methods show a good predictive ability under a zero pressure gradient, with the numerical method providing a complete velocity profile through the laminar sub-layer down to the wall. This work is of practical interest to computational fluid dynamic practitioners for generating an equilibrium thick turbulent boundary layer at the computational domain inflow. Copyright © 2009 by A. Rona.
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15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), 2009Author affiliation
/Organisation/COLLEGE OF SCIENCE AND ENGINEERING/Department of EngineeringSource
15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), 2009, Miami, FloridaVersion
- AM (Accepted Manuscript)
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15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference)Publisher
American Institute of Aeronautics and Astronautics (AIAA)isbn
9781563479748Copyright date
2009Available date
2016-02-24Publisher DOI
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http://arc.aiaa.org/doi/abs/10.2514/6.2009-3272Language
enAdministrator link
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