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dc.contributor.author유지형-
dc.date.accessioned2022-12-05T05:25:04Z-
dc.date.available2022-12-05T05:25:04Z-
dc.date.issued2022-05-
dc.identifier.citationJournal of Engineering for Gas Turbines and Power, v. 144, NO. 5, article no. 051011 EN, Page. 1-9en_US
dc.identifier.issn0742-4795;1528-8919en_US
dc.identifier.urihttps://asmedigitalcollection.asme.org/gasturbinespower/article/144/5/051011/1131138/Modal-Decomposition-Analysis-of-Combustionen_US
dc.identifier.urihttps://repository.hanyang.ac.kr/handle/20.500.11754/177943-
dc.description.abstractIn this work, the growth regime of combustion instability was studied by analyzing 10 kHz OH planar laser-induced fluorescence (PLIF) images through a combination of dynamic mode decomposition (DMD) and spectral proper orthogonal decomposition (SPOD) methods. Combustion instabilities were induced in a mesoscale burner array through an external speaker at an imposed perturbation frequency of 210 Hz. During the transient growth phase of combustion instability, 10 kHz OH PLIF imaging was employed to capture spatially and temporally resolved flame dynamics. Increased acoustic perturbations prevented flame reignition in the central recirculation zone and eventually led to the flame being extinguished inward from the outer burner array elements. Coherent modes and their growth rates were obtained from DMD spectral analyses of high-speed OH PLIF images. Positive growth rates were observed at the forcing frequency during the growth regime. Coherent structures, closely associated with thermoacoustic instability, were extracted using an appropriate SPOD filter operation to identify mode structures that correlate to physical phenomena such as shear layer instability and flame response to longitudinal acoustic forcing. Overall, a combination of DMD and SPOD was shown to be effective at analyzing the onset and propagation of combustion instabilities, particularly under transient burner operations.en_US
dc.description.sponsorshipThe authors of this work would like to acknowledge the support of Office of Naval Research through ONR Grant No. N00014-17-1-2538 with Dr. Steven Martens as program manager. Office of Naval Research (Grant No. N00014-17-1-2538; Funder ID: 10.13039/100000006).en_US
dc.languageenen_US
dc.publisherAmerican Society of Mechanical Engineers (ASME)en_US
dc.subjectmesoscale burner arrayen_US
dc.subjectswirl stabilized flameen_US
dc.subjectplanar laser induced fluorescenceen_US
dc.subjectdynamic mode decompositionen_US
dc.subjectspectral proper orthogonal decompositionen_US
dc.subjectcoherent modesen_US
dc.titleModal Decomposition Analysis of Combustion Instability Due to External Perturbation in a Mesoscale Burner Arrayen_US
dc.typeArticleen_US
dc.relation.no5-
dc.relation.volume144-
dc.identifier.doi10.1115/1.4053445en_US
dc.relation.page1-9-
dc.relation.journalJournal of Engineering for Gas Turbines and Power-
dc.contributor.googleauthorChoi, Jeongan-
dc.contributor.googleauthorRajasegar, Rajavasanth-
dc.contributor.googleauthorLiu, Qili-
dc.contributor.googleauthorLee, Tonghun-
dc.contributor.googleauthorYoo, Ji hyung-
dc.sector.campusS-
dc.sector.daehak공과대학-
dc.sector.department미래자동차공학과-
dc.identifier.pidjihyungyoo-
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COLLEGE OF ENGINEERING[S](공과대학) > AUTOMOTIVE ENGINEERING(미래자동차공학과) > Articles
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