Thermal boundary layers in turbulent Rayleigh-B\'enard convection with rough surfaces

TL;DR

This study provides detailed measurements of near-wall temperature fields in turbulent Rayleigh-Bénard convection with rough surfaces, revealing how roughness enhances heat transfer and influences the transition to turbulence.

Contribution

It offers the first high-resolution experimental insights into the local heat transfer mechanisms at rough surfaces in turbulent convection.

Findings

Heat flux enhancement linked to increased local heat transfer coefficient.

Transition in heat transfer scaling occurs at lower Ra with rough surfaces.

Early laminar-turbulent boundary layer transition due to surface roughness.

Abstract

We present highly resolved measurements of the near-wall temperature field in thermally driven convection at a rough surface. Our measurements have been undertaken in a very large experimental facility called the "Barrel of Ilmenau". They provide a unique insight into the local transport process at the interface between a hot solid surface and a surrounding fluid. In order to probe the near-wall temperature field, we used a tiny micro-thermistor of 130 $\mu$m in diameter and 330 $\mu$m in length with a response time $\tau_{70}$ of less than 150 ms. This sensor is forty times smaller than the thickness of the boundary layer, and it permits a resolution better than the typical Kolmogorov micro-scales that appear in our experiment. We demonstrate that the heat flux enhancement generally observed at rough surfaces, basically results from an increase of the local heat transfer coefficient at the top of the roughness elements. We also shed light on the detailed mechanism of the transition in the scaling of the global heat transfer relation $Nu\sim Ra^{\gamma}$ that has been observed beyond a critical Ra number $Ra_c$. In turbulent Rayleigh-B\'enard convection with rough surfaces, it already appears at $Ra_c\approx 10^{10}$ [Tisserand et al.{\em Phys. Fluids \/} 23, 015105(2011)] while, for smooth plates, it has been predicted at $Ra_c\approx 10^{14}$ [[Grossmann \& Lohse {\em Phys. Rev. Lett.\/} {\bf 86}, 3316(2001)]. We found this transition at rough surfaces to be attributed to an earlier laminar-turbulent transition of the boundary layer at the top of the roughness elements as well as to a modification of the temperature field in between the obstacles.