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

Jeffrey Santner, Xueliang Yang, Qian 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

    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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  • Cite this

    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] American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2015-0416