Published January 1, 2016
| Version v1
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Scaling and statistics of large-defect adverse pressure gradient turbulent boundary layers
- 1. Istanbul Tech Univ, Fac Aeronaut & Astronaut, TR-34469 Istanbul, Turkey
- 2. Univ Laval, Dept Mech Engn, Quebec City, PQ G1V 0A6, Canada
- 3. Univ Politecn Madrid, Sch Aeronaut, E-28040 Madrid, Spain
- 4. Monash Univ, Dept Mech & Aerosp Engn, Melbourne, Vic 3800, Australia
Description
The purpose of this article is to test similarity laws and scaling ideas, as well as characterize turbulence behaviour of large-defect adverse-pressure gradient turbulent boundary layers using six experimental and numerical databases including a new direct numerical simulation of a strongly decelerated non-equilibrium turbulent boundary layer. In the latter flow, at a moderate Reynolds number, the mean velocity profiles depart from the classical law of the wall throughout the inner region including in the viscous sublayer and they do not follow the log law. However, the agreement is excellent with the extended law of the wall that accounts for the pressure gradient for the viscous sublayer. The Reynolds stress components are not self-similar in the viscous sublayer when the velocity defect is important, but they scale reasonably well with the pressure-viscous scales.
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