posted on 2009-11-03, 14:36authored byAldo 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 a low and moderate adverse pressure gradient. Comparison
against experimental and DNS data show a good predictive ability under a zero
pressure gradient and a moderate adverse pressure gardient, with the numerical
method providing a complete velocity profile through the laminar sub-layer
down to the wall. The application of the method is useful to computational fluid
dynamic practitioners for generating an equilibrium thick turbulent boundary
layer at the computational domain inflow.
History
Citation
CEAS 2009 European Air and Space Conference, Manchester, 26-29 October 2009, Proceedings of
Published in
CEAS 2009 European Air and Space Conference
Publisher
Council of European Aerospace Societies (CEAS)
Available date
2009-11-03
Publisher version
http://www.ceas.org/
Notes
This is the author's final draft of the paper presented at CEAS 2009 European Air and Space Conference, Manchester, 26-29 October 2009. Further information about CEAS events can be found at http://www.ceas.org/