Jacobitz, Frank und Sysyn, Ian und Ryan, Jacob und Comfort, Jack und Poole, Dylan und Bonner, Patrick und Lemarechal, Jonathan und 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), Seiten 1-17. Elsevier. doi: 10.1016/j.ijheatfluidflow.2024.109656. ISSN 0142-727X.
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Offizielle URL: https://doi.org/10.1016/j.ijheatfluidflow.2024.109656
Kurzfassung
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.
elib-URL des Eintrags: | https://elib.dlr.de/212392/ | ||||||||||||||||||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||||||||||||||
Zusätzliche Informationen: | Article No. 109656 Open Access Artikel. https://www.sciencedirect.com/science/article/pii/S0142727X24003813?via%3Dihub | ||||||||||||||||||||||||||||||||||||
Titel: | On the interaction of a laminar heated boundary layer with a roughness element: A comparison of experiments and simulations for steady flow | ||||||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | März 2025 | ||||||||||||||||||||||||||||||||||||
Erschienen in: | International Journal of Heat and Fluid Flow | ||||||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||||||||||||||||||||||
Band: | 112 | ||||||||||||||||||||||||||||||||||||
DOI: | 10.1016/j.ijheatfluidflow.2024.109656 | ||||||||||||||||||||||||||||||||||||
Seitenbereich: | Seiten 1-17 | ||||||||||||||||||||||||||||||||||||
Herausgeber: |
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Verlag: | Elsevier | ||||||||||||||||||||||||||||||||||||
ISSN: | 0142-727X | ||||||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||||||
Stichwörter: | Roughness Element; Laminar Boundary Layer; Heated Surface; Temperature-Sensitive Paint; Numerical Simulation | ||||||||||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||||||||||
HGF - Programmthema: | Effizientes Luftfahrzeug | ||||||||||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | L EV - Effizientes Luftfahrzeug | ||||||||||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Virtuelles Flugzeug und Validierung | ||||||||||||||||||||||||||||||||||||
Standort: | Göttingen | ||||||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren, GO | ||||||||||||||||||||||||||||||||||||
Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||||||||||||||||||
Hinterlegt am: | 19 Feb 2025 13:20 | ||||||||||||||||||||||||||||||||||||
Letzte Änderung: | 19 Feb 2025 13:27 |
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