Asli, Majid und Stathopoulos, Panagiotis und Paschereit, Christian Oliver (2020) Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor. In: ASME Turbo Expo 2020 Turbomachinery Technical Conference and Exposition. ASME Turbo Expo 2020 Turbomachinery Technical Conference and Exposition, 2020-09-21 - 2020-09-25, Online-Veranstaltung. doi: 10.1115/1.4049188.
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Kurzfassung
Any outlet restriction downstream of Pressure Gain Combustion (PGC), such as turbine blades, affects its flow field and may cause additional thermodynamic losses. The unsteadiness in the form of pressure, temperature and velocity vector fluctuations has a negative impact on the operation of conventional turbines. Additionally, experimental measurements and data acquisition present researchers with challenges that have to do mostly with the high temperature exhaust of PGC and the high frequency of its operation. Nevertheless, numerical simulations can provide important insights into PGC exhaust flow and its interaction with turbine blades. In this paper, a Rotating Detonation Combustor (RDC) and a row of nozzle guide vanes have been modeled based on the data from literature and an available experimental setup. URANS simulations were done for five guide vane configurations with different geometrical parameters to investigate the effect of solidity and blade type representing different outlet restrictions on the RDC exhaust flow. The results analyzed the connection between total pressure loss and the vanes solidity and thickness to chord ratio. It is observed that more than 57% of the upstream velocity angle fluctuation amplitude was damped by the vanes. Furthermore, the area reduction was found to be the significant driving factor for damping the velocity angle fluctuations, whether in the form of solidity or thickness on chord ratio increment. This RDC exhaust flow investigation is an important primary step from a turbomachinery standpoint, which provided details of blade behavior in such an unsteady flow field.
elib-URL des Eintrags: | https://elib.dlr.de/139560/ | ||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||
Titel: | Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor | ||||||||||||||||
Autoren: |
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Datum: | 2020 | ||||||||||||||||
Erschienen in: | ASME Turbo Expo 2020 Turbomachinery Technical Conference and Exposition | ||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||
Open Access: | Ja | ||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||
DOI: | 10.1115/1.4049188 | ||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||
Stichwörter: | turbine design, pressure gain combustion, CFD, gas turbines | ||||||||||||||||
Veranstaltungstitel: | ASME Turbo Expo 2020 Turbomachinery Technical Conference and Exposition | ||||||||||||||||
Veranstaltungsort: | Online-Veranstaltung | ||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||
Veranstaltungsbeginn: | 21 September 2020 | ||||||||||||||||
Veranstaltungsende: | 25 September 2020 | ||||||||||||||||
HGF - Forschungsbereich: | Energie | ||||||||||||||||
HGF - Programm: | Energieeffizienz, Materialien und Ressourcen | ||||||||||||||||
HGF - Programmthema: | keine Zuordnung | ||||||||||||||||
DLR - Schwerpunkt: | Energie | ||||||||||||||||
DLR - Forschungsgebiet: | E SP - Energiespeicher | ||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | E - Dekarbonisierte Industrieprozesse (alt) | ||||||||||||||||
Standort: | Cottbus | ||||||||||||||||
Institute & Einrichtungen: | Institut für CO2-arme Industrieprozesse | ||||||||||||||||
Hinterlegt von: | Klinkmüller, Maike | ||||||||||||||||
Hinterlegt am: | 04 Jan 2021 10:56 | ||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:40 |
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