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dc.contributor.authorHabib, Mohamed A. M.
dc.contributor.authorTaamallah, Soufien
dc.contributor.authorLaBry, Zachary A
dc.contributor.authorGhoniem, Ahmed F
dc.contributor.authorShanbhogue, Santosh
dc.date.accessioned2017-03-06T15:55:00Z
dc.date.available2017-03-06T15:55:00Z
dc.date.issued2014-12
dc.date.submitted2014-10
dc.identifier.issn0742-4795
dc.identifier.urihttp://hdl.handle.net/1721.1/107189
dc.description.abstractIn this paper, we conduct an experimental investigation to study the link between the flame macroscale structure—or flame brush spatial distribution—and thermo-acoustic instabilities, in a premixed swirl-stabilized dump combustor. We operate the combustor with premixed methane–air in the range of equivalence ratio (φ) from the lean blowout limit to φ=0.75. First, we observe the different dynamic modes in this lean range as φ is raised. We also document the effect of φ on the flame macrostructure. Next, we examine the correspondence between dynamic mode transitions and changes in flame macrostructure. To do so, we modify the combustor length—by downstream truncation—without changing the underlying flow upstream. Thus, the resonant frequencies of the geometry are altered allowing for decoupling the heat release rate fluctuations and the acoustic feedback. Mean flame configurations in the modified combustor and for the same range of equivalence ratio are examined, following the same experimental protocol. It is found that not only the same sequence of flame macrostructures is observed in both combustors but also that the transitions occur at a similar set of equivalence ratio. In particular, the appearance of the flame in the outside recirculation zone (ORZ) in the long combustor—which occurs simultaneously with the onset of instability at the fundamental frequency—happens at similar φ when compared to the short combustor, but without being in latter case accompanied by a transition to thermo-acoustic instability. Then, we interrogate the flow field by analyzing the streamlines, mean, and rms velocities for the nonreacting flow and the different flame types. Finally, we focus on the transition of the flame to the ORZ in the acoustically decoupled case. Our analysis of this transition shows that it occurs gradually with an intermittent appearance of a flame in the ORZ and an increasing probability with φ. The spectral analysis of this phenomenon—we refer to as “ORZ flame flickering”—shows the presence of unsteady events occurring at two distinct low frequency ranges. A broad band at very low frequency in the range ∼(1 Hz–10 Hz) associated with the expansion and contraction of the inner recirculation zone (IRZ) and a narrow band centered around 28 Hz which is the frequency of rotation of the flame as it is advected by the ORZ flow.en_US
dc.description.sponsorshipKing Fahd University of Petroleum and Minerals (Grant R12-CE-10)en_US
dc.description.sponsorshipKing Abdullah University of Science and Technology (Grant KUS-110-010-01)en_US
dc.language.isoen_US
dc.publisherAmerican Society of Mechanical Engineersen_US
dc.relation.isversionofhttp://dx.doi.org/10.1115/1.4029173en_US
dc.rightsArticle is made available in accordance with the publisher's policy and may be subject to US copyright law. Please refer to the publisher's site for terms of use.en_US
dc.sourceAmerican Society of Mechanical Engineers (ASME)en_US
dc.titleCorrespondence Between “Stable” Flame Macrostructure and Thermo-acoustic Instability in Premixed Swirl-Stabilized Turbulent Combustionen_US
dc.typeArticleen_US
dc.identifier.citationTaamallah, Soufien et al. “Correspondence Between ‘Stable’ Flame Macrostructure and Thermo-Acoustic Instability in Premixed Swirl-Stabilized Turbulent Combustion.” Journal of Engineering for Gas Turbines and Power 137.7 (2015): 071505.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineeringen_US
dc.contributor.mitauthorTaamallah, Soufien
dc.contributor.mitauthorLaBry, Zachary A
dc.contributor.mitauthorGhoniem, Ahmed F
dc.contributor.mitauthorShanbhogue, Santosh
dc.relation.journalJournal of Engineering for Gas Turbines and Poweren_US
dc.eprint.versionFinal published versionen_US
dc.type.urihttp://purl.org/eprint/type/JournalArticleen_US
eprint.statushttp://purl.org/eprint/status/PeerRevieweden_US
dspace.orderedauthorsTaamallah, Soufien; LaBry, Zachary A.; Shanbhogue, Santosh J.; Habib, Mohamed A. M.; Ghoniem, Ahmed F.en_US
dspace.embargo.termsNen_US
dc.identifier.orcidhttps://orcid.org/0000-0001-8298-8857
dc.identifier.orcidhttps://orcid.org/0000-0001-8730-272X
mit.licensePUBLISHER_POLICYen_US


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