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dc.contributor.authorHernandez Perez, Francisco
dc.contributor.authorIm, Hong G.
dc.contributor.authorTingas, Efstathios Al
dc.date.accessioned2020-11-05T12:20:08Z
dc.date.available2020-11-05T12:20:08Z
dc.date.issued2020-01-05
dc.identifier.citationHernandez Perez, F. E., Im, H. G., & Tingas, A. E. (2020). Computational investigation of rod-stabilized laminar premixed hydrogen–methane–air flames. AIAA Scitech 2020 Forum. doi:10.2514/6.2020-1659
dc.identifier.isbn9781624105951
dc.identifier.doi10.2514/6.2020-1659
dc.identifier.urihttp://hdl.handle.net/10754/665842
dc.description.abstractA computational study of steady, rod-stabilized, inverted, lean, CH4–air and H2–CH4–air flames is conducted. For the CH4–air flames, either decreasing the inlet equivalence ratio or increasing the mean inflow velocity leads to a larger standoff distance, and below a critical value of the inlet equivalence ratio or above a critical value of the inflow velocity, the flame blows off. For the H2–CH4–air flames, decreasing the inlet equivalence ratio has similar effects as those on the CH4–air flames; however, increasing the inflow velocity reduces the standoff distance. Though counter-intuitive, the predicted behaviour of the flames is consistent with the experimental observations. Both the CH4–air and H2–CH4–air flames exhibit preferential diffusion effects such as superadiabatic temperatures and local equivalence ratio variations, which are more pronounced for the H2–CH4–air flames, displaying non-uniform and localized consumption rates of the fuel components. The strong diffusion of H2 plays an important role to maintain and even strengthen the reaction processes in the anchoring region and the counter-intuitive stabilization/blow-off of the H2–CH4–air flames.
dc.description.sponsorshipThis work was supported by King Abdullah University of Science and Technology (KAUST). Computational resources were provided by the KAUST Supercomputing Laboratory (KSL).
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)
dc.relation.urlhttps://arc.aiaa.org/doi/10.2514/6.2020-1659
dc.rightsArchived with thanks to American Institute of Aeronautics and Astronautics
dc.titleComputational investigation of rod-stabilized laminar premixed hydrogen–methane–air flames
dc.typeConference Paper
dc.contributor.departmentClean Combustion Research Center
dc.contributor.departmentPhysical Science and Engineering (PSE) Division
dc.contributor.departmentMechanical Engineering Program
dc.conference.date2020-01-06 to 2020-01-10
dc.conference.nameAIAA Scitech Forum, 2020
dc.conference.locationOrlando, FL, USA
dc.eprint.versionPost-print
dc.contributor.institutionEngineering and Aviation, Perth College, University of the Highlands and Islands (UHI), Crieff Road, Perth, PH1 2NX, United Kingdom
dc.identifier.volume1 PartF
kaust.personHernandez Perez, Francisco
kaust.personIm, Hong G.
dc.identifier.eid2-s2.0-85092404030
refterms.dateFOA2020-11-05T12:46:06Z
kaust.acknowledged.supportUnitKAUST Supercomputing Laboratory (KSL)
dc.date.published-online2020-01-05
dc.date.published-print2020-01-06


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