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On the generation of the mean velocityprofile for turbulent boundary layers with pressuregradient under equilibriumconditions

Published online by Cambridge University Press:  27 January 2016

A. Rona ,
M. Monti  and
C. Airiau
A. Rona*
Affiliation:
Department of Engineering, University of Leicester, Leicester, UK
M. Monti
Affiliation:
Department of Engineering, University of Leicester, Leicester, UK
C. Airiau
Affiliation:
Institut de Mécanique des Fluides de Toulouse, Université de Toulouse, Toulouse, France
*
ar45@le.ac.uk
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Abstract

The generation of a fully turbulent boundary layerprofile is investigated using analytical andnumerical methods over the Reynolds number range 422≤ Reθ ≤ 31,000. The numerical method usesa new mixing length blending function. Thepredictions are validated against reference windtunnel measurements under zero streamwise pressuregradient. The methods are then tested for low andmoderate adverse pressure gradients. Comparisonagainst experiment and DNS data show a goodpredictive ability under zero pressure gradient andmoderate adverse pressure gradient, with bothmethods providing a complete velocity profilethrough the viscous sub-layer down to the wall.These methods are useful computational fluid dynamictools for generating an equilibrium thick turbulentboundary layer at the computational domaininflow.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 116 , Issue 1180 , June 2012 , pp. 569 - 598
Copyright
Copyright © Royal Aeronautical Society 2012 

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