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On the generation of the mean velocity profile for turbulent boundary layers with pressure gradient under equilibrium conditions

journal contribution
posted on 2012-07-12, 14:36 authored by Aldo Rona, M. Monti, C. Airiau
The generation of a fully turbulent boundary layer profile is investigated using analytical and numerical methods over the Reynolds number range 422 ≤ Reѳ ≤ 31,000. The numerical method uses a new mixing length blending function. The predictions are validated against reference wind tunnel measurements under zero streamwise pressure gradient. The methods are then tested for low and moderate adverse pressure gradients. Comparison against experiment and DNS data show a good predictive ability under zero pressure gradient and moderate adverse pressure gradient, with both methods providing a complete velocity profile through the viscous sub-layer down to the wall. These methods are useful computational fluid dynamic tools for generating an equilibrium thick turbulent boundary layer at the computational domain inflow.

History

Citation

The Aeronautical Journal, 2012, 116 (1180)

Author affiliation

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

Version

  • AM (Accepted Manuscript)

Published in

The Aeronautical Journal

Publisher

Royal Aeronautical Society

issn

0001-9240

Copyright date

2012

Publisher version

http://aerosociety.com/News/Publications/Aero-Journal/Online

Notes

Embargo length currently unknown. Permission to make the text available has been requested from the publisher and the full text may be made available once this has been received.

Language

en

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