Jacobitz, Frank and Sysyn, Ian and Ryan, Jacob and Comfort, Jack and Poole, Dylan and Bonner, Patrick and Lemarechal, Jonathan and Costantini, Marco (2025) On the interaction of a laminar heated boundary layer with a roughness element: A comparison of experiments and simulations for steady flow. International Journal of Heat and Fluid Flow, 112 (109656), pp. 1-17. Elsevier. doi: 10.1016/j.ijheatfluidflow.2024.109656. ISSN 0142-727X.
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Official URL: https://doi.org/10.1016/j.ijheatfluidflow.2024.109656
Abstract
The aim of this study is a direct comparison of experimental and simulation results of two flows, a laminar boundary layer developing on a flat heated plate and the interaction of a laminar boundary layer with a single cylindrical roughness element of small aspect ratio with a height similar to the boundary layer thickness. The experiments were performed in a water channel using temperature-sensitive paint (TSP) on a heated flat plate on which the boundary layer develops. The numerical simulations are meant to complement the experimental data, allowing for a direct comparison with the experiment and adding additional information not easily accessible from the experiment. In the case of the laminar boundary layer developing over a flat heated surface, experimental TSP measurements and simulation results of the surface temperature show strong agreement and a correlation coefficient for the two temperature fields of 0.99 is obtained. In the case of a laminar boundary layer interacting with a low aspect ratio roughness element, the comparison between experimental and numerical data revealed the role played by buoyancy effects even at the small implemented temperature differences between surface and fluid. With consideration of buoyancy in the simulations, again good agreement between the experimental and simulation results is obtained with a correlation coefficient of 0.95 for the respective temperature fields. The complex vortical system identified in the flow field via the simulations was shown to be consistent with the thermal footprints measured on the heated wall in the experiments.
| Item URL in elib: | https://elib.dlr.de/212392/ | ||||||||||||||||||||||||||||||||||||
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| Document Type: | Article | ||||||||||||||||||||||||||||||||||||
| Additional Information: | Article No. 109656 Open Access Artikel. https://www.sciencedirect.com/science/article/pii/S0142727X24003813?via%3Dihub | ||||||||||||||||||||||||||||||||||||
| Title: | On the interaction of a laminar heated boundary layer with a roughness element: A comparison of experiments and simulations for steady flow | ||||||||||||||||||||||||||||||||||||
| Authors: |
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| Date: | March 2025 | ||||||||||||||||||||||||||||||||||||
| Journal or Publication Title: | International Journal of Heat and Fluid Flow | ||||||||||||||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||||||||||||||
| Open Access: | Yes | ||||||||||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||||||||||||||||||
| Volume: | 112 | ||||||||||||||||||||||||||||||||||||
| DOI: | 10.1016/j.ijheatfluidflow.2024.109656 | ||||||||||||||||||||||||||||||||||||
| Page Range: | pp. 1-17 | ||||||||||||||||||||||||||||||||||||
| Editors: |
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| Publisher: | Elsevier | ||||||||||||||||||||||||||||||||||||
| ISSN: | 0142-727X | ||||||||||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||||||||||
| Keywords: | Roughness Element; Laminar Boundary Layer; Heated Surface; Temperature-Sensitive Paint; Numerical Simulation | ||||||||||||||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||||||||||||||
| HGF - Program Themes: | Efficient Vehicle | ||||||||||||||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||||||||||||||
| DLR - Program: | L EV - Efficient Vehicle | ||||||||||||||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Virtual Aircraft and Validation | ||||||||||||||||||||||||||||||||||||
| Location: | Göttingen | ||||||||||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Experimental Methods, GO | ||||||||||||||||||||||||||||||||||||
| Deposited By: | Micknaus, Ilka | ||||||||||||||||||||||||||||||||||||
| Deposited On: | 19 Feb 2025 13:20 | ||||||||||||||||||||||||||||||||||||
| Last Modified: | 19 Feb 2025 13:27 |
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