Morsbach, Christian und Bergmann, Michael und Klose, Björn und Brakmann, Robin und Schroll, Michael und Carvalho, Francisco und Willert, Christian und Kügeler, Edmund (2026) Stabilizing the Jet: High-Fidelity Simulation of Advanced Impingement Cooling Using a Non-Conformal Discontinuous Galerkin Method. In: 71th ASME Turbo Expo 2026: Turbomachinery Technical Conference and Exposition, GT 2026. ASME Turbo Expo 2026: Turbomachinery Technical Conference and Exposition, 2026-06-15 - 2026-06-19, Mailand, Italien.
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Kurzfassung
In order to investigate jet impingement flows with complex geometry, we present an extension of a high-order Discontinuous Galerkin Spectral Element Method to non-conformal hexahedral meshes with 2-1 and 4-1 element connections. The convergence order of the method is verified and its suitability for the simulation of turbulent flows is validated using generic flows with known reference solutions. Using the new method, we obtain a new reference data set for a multi-jet impingement configuration consisting of 9 jets injected into a square channel. The present simulations include the plenum above the pipe inlet and it is shown how this improves the consistency with the experimentally investigated configuration in terms of jet velocity profile compared to previous simulations without the plenum. Due to the changed velocity profile, the downstream jets are deflected more strongly and the average Nusselt number is reduced while the unsteady dynamics remain qualitatively consistent. Finally, the effect of placing U-shaped flow guides on the hole plate is validated with particle image velocimetry data and their effect on the average and instantaneous heat transfer characteristics is discussed.
| elib-URL des Eintrags: | https://elib.dlr.de/226411/ | ||||||||||||||||||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||||||
| Titel: | Stabilizing the Jet: High-Fidelity Simulation of Advanced Impingement Cooling Using a Non-Conformal Discontinuous Galerkin Method | ||||||||||||||||||||||||||||||||||||
| Autoren: |
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| Datum: | 15 September 2026 | ||||||||||||||||||||||||||||||||||||
| Erschienen in: | 71th ASME Turbo Expo 2026: Turbomachinery Technical Conference and Exposition, GT 2026 | ||||||||||||||||||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||||||||||||||
| Stichwörter: | large eddy simulation, impingement cooling, discontinuous Galerkin, non-conformal mesh | ||||||||||||||||||||||||||||||||||||
| Veranstaltungstitel: | ASME Turbo Expo 2026: Turbomachinery Technical Conference and Exposition | ||||||||||||||||||||||||||||||||||||
| Veranstaltungsort: | Mailand, Italien | ||||||||||||||||||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||||||
| Veranstaltungsbeginn: | 15 Juni 2026 | ||||||||||||||||||||||||||||||||||||
| Veranstaltungsende: | 19 Juni 2026 | ||||||||||||||||||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||||||||||
| HGF - Programmthema: | Umweltschonender Antrieb | ||||||||||||||||||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||||||||||
| DLR - Forschungsgebiet: | L CP - Umweltschonender Antrieb | ||||||||||||||||||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Virtuelles Triebwerk, E - Verbrennungs- und Kraftwerkssysteme | ||||||||||||||||||||||||||||||||||||
| Standort: | Göttingen , Köln-Porz | ||||||||||||||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Antriebstechnik > Numerische Methoden Institut für Antriebstechnik > Turbine Institut für Test und Simulation für Gasturbinen > Virtuelle Turbine und numerische Methoden Institut für Antriebstechnik > Triebwerksmesstechnik | ||||||||||||||||||||||||||||||||||||
| Hinterlegt von: | Morsbach, Christian | ||||||||||||||||||||||||||||||||||||
| Hinterlegt am: | 28 Aug 2026 13:13 | ||||||||||||||||||||||||||||||||||||
| Letzte Änderung: | 28 Aug 2026 13:13 |
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