Greifenstein, M. ; Heinze, J. ; Willert, C. ; Voigt, L. ; Zedda, M. ; Richter, C. ; Dreizler, A. (2024)
Time-resolved temperature profile measurements in the exhaust of a single sector gas turbine combustor at realistic operating conditions.
In: Experiments in Fluids : Experimental Methods and their Applications to Fluid Flow, 2020, 61 (8)
doi: 10.26083/tuprints-00023903
Artikel, Zweitveröffentlichung, Verlagsversion
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Kurzbeschreibung (Abstract)
Records of the time-varying temperature profile at flight relevant operating conditions are acquired at the exit of a combustion chamber fitted with a staged, lean-burn fuel injector using high-speed laser induced fluorescence (LIF) at a sample rate of 10 kHz. Temperatures are estimated from the concentration dependent fluorescence of the hydroxyl (OH) radical under the assumption of local equilibrium. Beyond the time-series analysis, the acquired data is correlated with simultaneously acquired OH chemiluminescence sampled in the primary zone near the fuel injector. These analyses reveal a strong influence from the precessing vortex core, originating in the primary zone, on oscillations in the temperature profiles measured at the exit of the combustor.
Typ des Eintrags: | Artikel |
---|---|
Erschienen: | 2024 |
Autor(en): | Greifenstein, M. ; Heinze, J. ; Willert, C. ; Voigt, L. ; Zedda, M. ; Richter, C. ; Dreizler, A. |
Art des Eintrags: | Zweitveröffentlichung |
Titel: | Time-resolved temperature profile measurements in the exhaust of a single sector gas turbine combustor at realistic operating conditions |
Sprache: | Englisch |
Publikationsjahr: | 30 April 2024 |
Ort: | Darmstadt |
Publikationsdatum der Erstveröffentlichung: | August 2020 |
Ort der Erstveröffentlichung: | Berlin ; Heidelberg |
Verlag: | Springer |
Titel der Zeitschrift, Zeitung oder Schriftenreihe: | Experiments in Fluids : Experimental Methods and their Applications to Fluid Flow |
Jahrgang/Volume einer Zeitschrift: | 61 |
(Heft-)Nummer: | 8 |
Kollation: | 12 Seiten |
DOI: | 10.26083/tuprints-00023903 |
URL / URN: | https://tuprints.ulb.tu-darmstadt.de/23903 |
Zugehörige Links: | |
Herkunft: | Zweitveröffentlichung DeepGreen |
Kurzbeschreibung (Abstract): | Records of the time-varying temperature profile at flight relevant operating conditions are acquired at the exit of a combustion chamber fitted with a staged, lean-burn fuel injector using high-speed laser induced fluorescence (LIF) at a sample rate of 10 kHz. Temperatures are estimated from the concentration dependent fluorescence of the hydroxyl (OH) radical under the assumption of local equilibrium. Beyond the time-series analysis, the acquired data is correlated with simultaneously acquired OH chemiluminescence sampled in the primary zone near the fuel injector. These analyses reveal a strong influence from the precessing vortex core, originating in the primary zone, on oscillations in the temperature profiles measured at the exit of the combustor. |
Freie Schlagworte: | Engineering Fluid Dynamics, Fluid- and Aerodynamics, Engineering Thermodynamics, Heat and Mass Transfer |
ID-Nummer: | Artikel-ID: 177 |
Status: | Verlagsversion |
URN: | urn:nbn:de:tuda-tuprints-239033 |
Sachgruppe der Dewey Dezimalklassifikatin (DDC): | 500 Naturwissenschaften und Mathematik > 530 Physik 600 Technik, Medizin, angewandte Wissenschaften > 620 Ingenieurwissenschaften und Maschinenbau |
Fachbereich(e)/-gebiet(e): | 16 Fachbereich Maschinenbau 16 Fachbereich Maschinenbau > Fachgebiet Reaktive Strömungen und Messtechnik (RSM) |
Hinterlegungsdatum: | 30 Apr 2024 11:15 |
Letzte Änderung: | 02 Mai 2024 07:44 |
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- Time-resolved temperature profile measurements in the exhaust of a single sector gas turbine combustor at realistic operating conditions. (deposited 30 Apr 2024 11:15) [Gegenwärtig angezeigt]
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