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dc.contributor.author
Solana Pérez, Roberto
dc.contributor.author
Shcherbanev, Serge
dc.contributor.author
Dharmaputra, Bayu
dc.contributor.author
Ciani, Andrea
dc.contributor.author
Noiray, Nicolas
dc.date.accessioned
2023-06-08T12:31:52Z
dc.date.available
2023-02-13T09:24:48Z
dc.date.available
2023-02-13T10:03:55Z
dc.date.available
2023-02-14T07:27:15Z
dc.date.available
2023-02-14T10:43:53Z
dc.date.available
2023-06-08T12:31:52Z
dc.date.issued
2023
dc.identifier.issn
1540-7489
dc.identifier.issn
1873-2704
dc.identifier.other
10.1016/j.proci.2022.08.014
en_US
dc.identifier.uri
http://hdl.handle.net/20.500.11850/598109
dc.identifier.doi
10.3929/ethz-b-000598109
dc.description.abstract
The combustion regime transition in a sequential burner (SB) supplied with H (48 kW) is experimentally studied during steady and transient operation. The test rig is a simplified model of an industrial sequential combustor featuring two-staged combustion chambers separated by a mixing section in which dilution air and fuel are injected. The temperature, velocity and composition of the hot vitiated gas flowing through the SB are defined by the products from the first stage (30 kW natural gas-air flame at equivalence ratio 0.7), and by the mass flow of dilution air. To study the combustion regime transition during steady operation of the combustor, is fixed at several values between 22 g/s and 7 g/s. For transient operation investigations, is suddenly changed between 20 and 7 g/s, which triggers a fast transition of the combustion mode. High-speed hydroxyl radicals OH chemiluminescence is used to characterize the combustion process, and optical emission spectroscopy (OES) and tunable diode laser absorption spectroscopy (TDLAS) are respectively used to extract mean and time-resolved temperatures of the vitiated gas in the SB. In particular, we investigate the transition from a propagation-driven turbulent flame anchored at the inlet of the sequential combustion chamber, to a flame stabilized by autoignition inside the mixing section of the burner when the dilution air mass flow is suddenly reduced. Zero-dimensional (0D) simulations are used to analyze the underlying combustion regime transition. A 0D reactor network is developed and calibrated with the experimental data. This simplified low-order model predicts well the flame location for both steady and transient operation. Moreover, the good agreement between the numerical results and the experimental data demonstrates that time-resolved TDLAS successfully enables measurement of small temperature variations in the vitiated flow associated with non-perfect mixing of the different streams in the SB.
en_US
dc.format
application/pdf
en_US
dc.language.iso
en
en_US
dc.publisher
Combustion Institute
en_US
dc.rights.uri
http://creativecommons.org/licenses/by/4.0/
dc.subject
Hydrogen
en_US
dc.subject
Autoignition
en_US
dc.subject
Sequential combustion
en_US
dc.subject
Hydrogen combustion
en_US
dc.title
Combustion regime transition of H2 flames during steady and transient operation of a sequential combustor
en_US
dc.type
Journal Article
dc.rights.license
Creative Commons Attribution 4.0 International
dc.date.published
2022-09-30
ethz.journal.title
Proceedings of the Combustion Institute
ethz.journal.volume
39
en_US
ethz.journal.issue
4
en_US
ethz.journal.abbreviated
Proc. Combust. Inst.
ethz.pages.start
4335
en_US
ethz.pages.end
4344
en_US
ethz.version.deposit
publishedVersion
en_US
ethz.grant
ThermoacOustic instabilities contRol in sequential Combustion cHambers
en_US
ethz.identifier.wos
ethz.identifier.scopus
ethz.publication.place
Pittsburgh, PA
en_US
ethz.publication.status
published
en_US
ethz.leitzahl
ETH Zürich::00002 - ETH Zürich::00012 - Lehre und Forschung::00007 - Departemente::02130 - Dep. Maschinenbau und Verfahrenstechnik / Dep. of Mechanical and Process Eng.::02668 - Inst. f. Energie- und Verfahrenstechnik / Inst. Energy and Process Engineering::09471 - Noiray, Nicolas / Noiray, Nicolas
en_US
ethz.leitzahl.certified
ETH Zürich::00002 - ETH Zürich::00012 - Lehre und Forschung::00007 - Departemente::02130 - Dep. Maschinenbau und Verfahrenstechnik / Dep. of Mechanical and Process Eng.::02668 - Inst. f. Energie- und Verfahrenstechnik / Inst. Energy and Process Engineering::09471 - Noiray, Nicolas / Noiray, Nicolas
en_US
ethz.tag
combustion dynamics
en_US
ethz.tag
hydrogen fuel
en_US
ethz.tag
gas turbines
en_US
ethz.grant.agreementno
820091
ethz.grant.agreementno
820091
ethz.grant.agreementno
820091
ethz.grant.fundername
EC
ethz.grant.fundername
EC
ethz.grant.fundername
EC
ethz.grant.funderDoi
10.13039/501100000780
ethz.grant.funderDoi
10.13039/501100000780
ethz.grant.funderDoi
10.13039/501100000780
ethz.grant.program
H2020
ethz.grant.program
H2020
ethz.grant.program
H2020
ethz.date.deposited
2023-02-13T09:24:48Z
ethz.source
FORM
ethz.eth
yes
en_US
ethz.availability
Open access
en_US
ethz.rosetta.installDate
2023-06-08T12:31:53Z
ethz.rosetta.lastUpdated
2024-02-02T23:57:43Z
ethz.rosetta.versionExported
true
ethz.COinS
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