Fritz, Stefan und Koppers, Felix und Hergt, Alexander und Bresemann, David und Eck, Mario und Peitsch, Dieter und Möller, Felix und Rückert, Roland (2025) Highly Aggressive Inter Compressor Duct With Active Flow Control Part 2: Numerical Validation of Pulsed Jet Actuators With Unsteady Simulations. In: 70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, GT 2025, Seiten 1-13. 70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, 2025-06-16 - 2025-06-20, Memphis, Tennessee, USA. doi: 10.1115/GT2025-152898. ISBN 978-079188887-2.
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Offizielle URL: https://asmedigitalcollection.asme.org/GT/proceedings-abstract/GT2025/88872/V011T33A003/1220784
Kurzfassung
The application of active flow control (AFC) methods in an inter compressor duct (ICD) offers the possibility of further length reduction while suppressing separations. In particular, pulsed jet actuators (PJAs) are advantageous because the pulsation enhances mixing processes. However, the PJAs require fluid that has already been compressed by the downstream high pressure compressor. Therefore, injecting this high momentum fluid from a downstream component makes this approach very expensive. Consequently, a highly optimized design is required to achieve the maximum separation suppression while minimizing the external energy. However, the numerical optimization requires steady simulations to find an optimum design in manageable time scales. Therefore, this study helps understanding if any aspects of unsteadiness are neglected by optimizing the PJA implementation with steady methods. Furthermore, the influence of the steady state assumption in the optimization is quantified. The influence of the unsteadiness of the PJA is investigated by comparing steady and unsteady simulations. The unsteady simulations include unsteady Reynolds-averaged Navier-Stokes and delayed detached-eddy simulation. The numerical simulations are validated against experimental data, obtained at the TU Berlin ICD test rig. After evaluating the different approaches, a conclusion is drawn on how unsteady flow control methods can be efficiently optimized. Consequently, the study shows that all the methods investigated have their advantages and disadvantages. Their use must be carefully selected according to the objective of the investigation.
| elib-URL des Eintrags: | https://elib.dlr.de/214910/ | ||||||||||||||||||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||||||
| Zusätzliche Informationen: | Die Veröffentlichung ist im Rahmen des Projektes RDuct im LuFo Förderprogramm (LuFo VI-2, Fördernummer 20Q2110) des Bundesministerium für Wirtschaft und Energie entstanden. | ||||||||||||||||||||||||||||||||||||
| Titel: | Highly Aggressive Inter Compressor Duct With Active Flow Control Part 2: Numerical Validation of Pulsed Jet Actuators With Unsteady Simulations | ||||||||||||||||||||||||||||||||||||
| Autoren: |
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| Datum: | 11 August 2025 | ||||||||||||||||||||||||||||||||||||
| Erschienen in: | 70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, GT 2025 | ||||||||||||||||||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||||||
| DOI: | 10.1115/GT2025-152898 | ||||||||||||||||||||||||||||||||||||
| Seitenbereich: | Seiten 1-13 | ||||||||||||||||||||||||||||||||||||
| ISBN: | 978-079188887-2 | ||||||||||||||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||||||||||||||
| Stichwörter: | unsteady simulations, inter compressor duct, active flow control | ||||||||||||||||||||||||||||||||||||
| Veranstaltungstitel: | 70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition | ||||||||||||||||||||||||||||||||||||
| Veranstaltungsort: | Memphis, Tennessee, USA | ||||||||||||||||||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||||||
| Veranstaltungsbeginn: | 16 Juni 2025 | ||||||||||||||||||||||||||||||||||||
| Veranstaltungsende: | 20 Juni 2025 | ||||||||||||||||||||||||||||||||||||
| Veranstalter : | The American Society of Mechanical Engineers | ||||||||||||||||||||||||||||||||||||
| 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 - Komponenten und Emissionen | ||||||||||||||||||||||||||||||||||||
| Standort: | Köln-Porz | ||||||||||||||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Antriebstechnik > Fan- und Verdichter Institut für Test und Simulation für Gasturbinen > Virtuelle Turbine und numerische Methoden | ||||||||||||||||||||||||||||||||||||
| Hinterlegt von: | Fritz, Stefan | ||||||||||||||||||||||||||||||||||||
| Hinterlegt am: | 27 Okt 2025 11:38 | ||||||||||||||||||||||||||||||||||||
| Letzte Änderung: | 27 Okt 2025 11:38 |
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