HP-mech: A high pressure kinetic mechanism for C2 flames with exhaust gas dilution

Jeffrey Santner, Xueliang Yang, Qiang Wang, Yiguang Ju, Xiaobo Shen

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Abstract

This work represents continued development of a high pressure combustion chemistry mechanism (HP-Mech) for C2 mixtures with exhaust gas recirculation (EGR) at Princeton University. New burning velocity measurements were performed for ethane flames using the expanding spherical flame method at pressures from 1 to 20 atm with carbon dioxide and water vapor dilution. By holding the adiabatic flame temperature constant with dilution, the chemical effects of these diluents are investigated. These new measurements, as well as previous work with acetylene and ethylene, are used to improve and validate HP-Mech for C2 fuels.

Original languageEnglish (US)
Title of host publication53rd AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103438
DOIs
StatePublished - Jan 1 2015
Event53rd AIAA Aerospace Sciences Meeting, 2015 - Kissimmee, United States
Duration: Jan 5 2015Jan 9 2015

Publication series

Name53rd AIAA Aerospace Sciences Meeting

Other

Other53rd AIAA Aerospace Sciences Meeting, 2015
CountryUnited States
CityKissimmee
Period1/5/151/9/15

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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    Santner, J., Yang, X., Wang, Q., Ju, Y., & Shen, X. (2015). HP-mech: A high pressure kinetic mechanism for C2 flames with exhaust gas dilution. In 53rd AIAA Aerospace Sciences Meeting [AIAA 2015-0416] (53rd AIAA Aerospace Sciences Meeting). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2015-0416