A Simulation Study of the Interaction of a Blasius Boundary Layer with a Roughness Element
ORAL
Abstract
Roughness elements on surfaces of transportation systems can contribute to the transition from laminar to turbulent flow, impacting the overall energy requirements due to increased drag, and improving the stability of lift forces. The present study considers the interaction of a Blasius Boundary Layer developing on a flat surface with a cylindrical roughness element of small aspect ratio and a height smaller than the local boundary layer thickness. Using Ansys CFD, the development of a horseshoe-shaped vortical structure around the roughness element as well as a recirculation zone directly downstream of the roughness element is observed. The simulations aim to reproduce previous experiments (J. Lemarechal et al., 2018) visualizing the flow structure through the use of temperature-sensitive paint (TSP) applied to a heated surface. The simulations and experiments qualitatively show the same vortical flow structure. A direct comparison of the surface temperatures in the roughness element’s wake region yields a correlation coefficient of 0.85, also indicating strong quantitative agreement between simulations and experiments. The temperature signature is also a good indicator for regions of high wall shear stress. due to the horseshoe-vortex.
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Authors
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Ian Sysyn
University of San Diego
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Patrick Bonner
University of San Diego
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Frank Jacobitz
University of San Diego
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Jonathan Lemarechal
German Aerospace Center (DLR)
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Marco Costantini
German Aerospace Center (DLR)