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dc.contributor.authorTingas, Efstathios Al
dc.contributor.authorKashtanov, Roman
dc.contributor.authorHernandez Perez, Francisco
dc.contributor.authorIm, Hong G.
dc.contributor.authorCiottoli, Pietro Paolo
dc.contributor.authorGalassi, Riccardo Malpica
dc.contributor.authorValorani, Mauro
dc.date.accessioned2020-12-31T08:26:13Z
dc.date.available2020-12-31T08:26:13Z
dc.date.issued2017-01-01
dc.identifier.urihttp://hdl.handle.net/10754/666784
dc.description.abstractIn the current study, tools generated from the computational singular perturbation (CSP) are used to analyze the dynamics that develops in a three-dimensional (3D) turbulent H2/air flame. On top of these tools, the recently proposed tangential stretch rate (TSR) approach is used to obtain physical understanding of the turbulent flame. The analysis is first conducted on a laminar premixed H2/air flame followed by the analysis of the 3D turbulent flame at three distinct time steps. Using algorithmic tools, the flame front was identified along with the dominant processes reaction and transport (diffusive/convective) processes. Furthermore, the overall role of kinetics/transport was determined at each part of the flame.
dc.publisherCombustion Institute
dc.relation.urlhttps://research.kaust.edu.sa/en/publications/dynamical-analysis-of-turbulent-premixed-hydrogenair-flames-in-th
dc.rightsArchived with thanks to Combustion Institute
dc.titleDynamical analysis of turbulent premixed hydrogen/air flames in the thin reaction zone regime
dc.typeConference Paper
dc.contributor.departmentKing Abdullah University of Science and Technology (KAUST), Thuwal-Jeddah, 23955-6900, Saudi Arabia
dc.contributor.departmentClean Combustion Research Center
dc.contributor.departmentPhysical Science and Engineering (PSE) Division
dc.contributor.departmentMechanical Engineering Program
dc.conference.date2017-12-10 to 2017-12-14
dc.conference.name11th Asia-Pacific Conference on Combustion, ASPACC 2017
dc.conference.locationSydney, NSW, AUS
dc.eprint.versionPre-print
dc.contributor.institutionMechanical Department of Aerospace Engineering, Universität der Bundeswehr München Neubiberg, Munich, 85577, Germany
dc.contributor.institutionMechanical and Aerospace Engineering Department, Sapienza University of Rome, Via Eudossiana, 18, Rome, 00184, Italy
dc.identifier.volume2017-December
kaust.personTingas, Efstathios Al
kaust.personKashtanov, Roman
kaust.personHernandez Perez, Francisco
kaust.personIm, Hong G.
dc.identifier.eid2-s2.0-85046656491


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