Maciel, Yvan und Knopp, Tobias und Saxton-Fox, Theresa und Ambrogi, Francesco (2026) Pressure Gradient Parameters for Turbulent Boundary Layers Capturing Non-Equilibrium Effects in Steady and Unsteady Flows. In: 57th AVT Panel Business Week AVT-425 Research Specialists’ Meeting (RSM) on Physics and Modeling of Flow Separation 2026. 57th AVT Panel Business Week AVT-425 Research Specialists’ Meeting (RSM) on Physics and Modeling of Flow Separation 2026, 2026-05-18 - 2026-05-21, Bordeaux, France.
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Offizielle URL: https://web-eur.cvent.com/event/b6c318cb-5da9-4522-ba0a-bccf8d2e9c0d/summary
Kurzfassung
We present two pressure gradient parameters designed to capture history effects in strongly nonequilibrium steady turbulent boundary layers, as well as history and memory effects in unsteady turbulent boundary layers where unsteady inertia forces are not dominant. The first parameter is defined as the Lagrangian (material) time average of the pressure gradient parameter βZS, computed for a fictitious particle traveling through the ensemble-averaged flow field. The second parameter is derived from a transport-relaxation differential equation. As the transport–relaxation parameter has not yet been extensively validated, the paper primarily focuses on the Lagrangian-based parameter. This cumulative parameter is assessed using seven strongly non-equilibrium TBLs, comprising four steady and three unsteady cases. In the steady cases, it captures the history effects of the pressure force reasonably well, outperforming two cumulative parameters from the literature and performing comparably to the one proposed by Gomez and McKeon (J. Fluid Mech., 1002:A20, 2025). Its main advantage, however, lies in its ability to capture history and memory effects in unsteady cases, provided that unsteady inertia forces remain secondary. Regarding the transport-relaxation pressure-gradient parameter, an initial application to a strongly decelerated boundary layer indicates behavior similar to that of the Lagrangian-based parameter.
| elib-URL des Eintrags: | https://elib.dlr.de/225594/ | ||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
| Titel: | Pressure Gradient Parameters for Turbulent Boundary Layers Capturing Non-Equilibrium Effects in Steady and Unsteady Flows | ||||||||||||||||||||
| Autoren: |
| ||||||||||||||||||||
| Datum: | 22 Juni 2026 | ||||||||||||||||||||
| Erschienen in: | 57th AVT Panel Business Week AVT-425 Research Specialists’ Meeting (RSM) on Physics and Modeling of Flow Separation 2026 | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| Herausgeber: |
| ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | Turbulent Boundary Layer; Pressure Gradient Parameter; Unsteady Flow; Lagrangian; | ||||||||||||||||||||
| Veranstaltungstitel: | 57th AVT Panel Business Week AVT-425 Research Specialists’ Meeting (RSM) on Physics and Modeling of Flow Separation 2026 | ||||||||||||||||||||
| Veranstaltungsort: | Bordeaux, France | ||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
| Veranstaltungsbeginn: | 18 Mai 2026 | ||||||||||||||||||||
| Veranstaltungsende: | 21 Mai 2026 | ||||||||||||||||||||
| Veranstalter : | NATO STO AVT | ||||||||||||||||||||
| 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 - Digitale Technologien | ||||||||||||||||||||
| Standort: | Göttingen | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > CASE, GO | ||||||||||||||||||||
| Hinterlegt von: | Knopp, Dr.rer.nat. Tobias | ||||||||||||||||||||
| Hinterlegt am: | 22 Jul 2026 12:04 | ||||||||||||||||||||
| Letzte Änderung: | 22 Jul 2026 12:04 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags