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Surrogate fuel analysis and reduction using computational singular perturbation

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dc.contributor.author Valorani, M en
dc.contributor.author Creta, F en
dc.contributor.author Brizzi, AL en
dc.contributor.author Najm, H en
dc.contributor.author Goussis, DA en
dc.date.accessioned 2014-03-01T02:51:49Z
dc.date.available 2014-03-01T02:51:49Z
dc.date.issued 2008 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/35671
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-78149421825&partnerID=40&md5=8468df693b8ec22e75e0758d7b03e066 en
dc.subject.other Auto-ignition process en
dc.subject.other Computational singular perturbation en
dc.subject.other Constant volumes en
dc.subject.other Equivalence ratios en
dc.subject.other High-temperature kinetics en
dc.subject.other Kinetic mechanism en
dc.subject.other Lean mixtures en
dc.subject.other Soot precursors en
dc.subject.other Surrogate fuels en
dc.subject.other Target species en
dc.subject.other Aerospace engineering en
dc.subject.other Internet protocols en
dc.subject.other Fuels en
dc.title Surrogate fuel analysis and reduction using computational singular perturbation en
heal.type conferenceItem en
heal.identifier.secondary 2008-1009 en
heal.publicationDate 2008 en
heal.abstract We follow the simplification procedure described in previous work to generate simplified kinetic mechanisms for the surrogate fuel proposed by Dagaut for jet fuels. A family of comprehensive mechanisms is produced at different pressures (1, 10, 20, and 40 atm) by analyzing the constant volume, adiabatic, spatially homogeneous, auto-ignition process of surrogate/air mixture at different equivalence ratios and initial temperatures. We identify the prevailing pathways of surrogate oxidation for low and high temperature kinetics for a lean mixture at 10 atm. We assess how the accuracy of the prediction of soot precursors changes with different choices of the set of target species. Copyright © 2008 by the American Institute of Aeronautics and Astronautics, Inc. en
heal.journalName 46th AIAA Aerospace Sciences Meeting and Exhibit en


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