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Generation of a turbulent boundary layer inflow for RANS simulations

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conference contribution
posted on 2016-02-24, 11:32 authored by Aldo Rona, M. Grottadaurea, M. Monti, C. Airiau, T. Gandhi
The 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.

History

Citation

15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), 2009

Author affiliation

/Organisation/COLLEGE OF SCIENCE AND ENGINEERING/Department of Engineering

Source

15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), 2009, Miami, Florida

Version

  • AM (Accepted Manuscript)

Published in

15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference)

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

isbn

9781563479748

Copyright date

2009

Available date

2016-02-24

Publisher version

http://arc.aiaa.org/doi/abs/10.2514/6.2009-3272

Language

en

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