Effect of flame response asymmetries on the modal patterns and collective states of a can-annular lean-premixed combustion system

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dc.contributor.authorGuan, Yuko
dc.contributor.authorLi, Larryko
dc.contributor.authorJegal, Hyunwookko
dc.contributor.authorKim, Kyu Taeko
dc.date.accessioned2023-06-14T03:00:11Z-
dc.date.available2023-06-14T03:00:11Z-
dc.date.created2022-11-13-
dc.date.created2022-11-13-
dc.date.created2022-11-13-
dc.date.issued2023-06-
dc.identifier.citationPROCEEDINGS OF THE COMBUSTION INSTITUTE, v.39, no.4, pp.4731 - 4739-
dc.identifier.issn1540-7489-
dc.identifier.urihttp://hdl.handle.net/10203/307255-
dc.description.abstractWe experimentally study the effect of rotational asymmetries in the flame response distribution on the thermoacoustic oscillations of four turbulent lean-premixed combustors coupled in a ring network. The asymmetries are created via different combinations of high-swirl (HS) and low-swirl (LS) nozzles. By analyzing the inter-combustor acoustic interactions in terms of discrete thermoacoustic modes, we find a variety of modal patterns: (i) global alternating push–pull modes emerge for most pair-wise asymmetric nozzle combinations, (ii) 2-can push–pull modes emerge for an alternating 2-fold symmetric nozzle combination, and (iii) strong mode localization and global push–push modes emerge when the HS nozzles outnumber the LS nozzles. Using a complex systems framework, we reinterpret these modal patterns as collective states, such as a weak breathing chimera, a weak anti-phase chimera, and in-phase/anti-phase synchronization. This study shows that changing the flame response distribution of a multi-combustor system, via changes in the nozzle swirl distribution, can induce a variety of modal patterns and collective states. This sets the stage for the potential use of rotational asymmetries in the passive control of thermoacoustic modes in can-annular combustion systems.-
dc.languageEnglish-
dc.publisherELSEVIER SCIENCE INC-
dc.titleEffect of flame response asymmetries on the modal patterns and collective states of a can-annular lean-premixed combustion system-
dc.typeArticle-
dc.identifier.wosid001020833900001-
dc.identifier.scopusid2-s2.0-85142809830-
dc.type.rimsART-
dc.citation.volume39-
dc.citation.issue4-
dc.citation.beginningpage4731-
dc.citation.endingpage4739-
dc.citation.publicationnamePROCEEDINGS OF THE COMBUSTION INSTITUTE-
dc.identifier.doi10.1016/j.proci.2022.08.095-
dc.contributor.localauthorKim, Kyu Tae-
dc.contributor.nonIdAuthorGuan, Yu-
dc.contributor.nonIdAuthorLi, Larry-
dc.description.isOpenAccessN-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorCan-annular-
dc.subject.keywordAuthorCombustion instability-
dc.subject.keywordAuthorComplex systems-
dc.subject.keywordAuthorGas turbines-
dc.subject.keywordAuthorThermoacoustics-
dc.subject.keywordPlusCROSS-TALK-
dc.subject.keywordPlusACOUSTIC INTERACTIONS-
dc.subject.keywordPlusSYNCHRONIZATION-
dc.subject.keywordPlusINSTABILITIES-
dc.subject.keywordPlusOSCILLATIONS-
dc.subject.keywordPlusDYNAMICS-
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