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    High-Pressure Oxy-Syngas Ignition Delay Times With CO2 Dilution: Shock Tube Measurements and Comparison of the Performance of Kinetic Mechanisms

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 002::page 21011
    Author:
    Barak, Samuel
    ,
    Ninnemann, Erik
    ,
    Neupane, Sneha
    ,
    Barnes, Frank
    ,
    Kapat, Jayanta
    ,
    Vasu, Subith
    DOI: 10.1115/1.4040904
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this study, syngas combustion was investigated behind reflected shock waves in CO2 bath gas to measure ignition delay times (IDT) and to probe the effects of CO2 dilution. New syngas data were taken between pressures of 34.58–45.50 atm and temperatures of 1113–1275 K. This study provides experimental data for syngas combustion in CO2 diluted environments: ignition studies in a shock tube (59 data points in 10 datasets). In total, these mixtures covered a range of temperatures T, pressures P, equivalence ratios φ, H2/CO ratio θ, and CO2 diluent concentrations. Multiple syngas combustion mechanisms exist in the literature for modeling IDTs and their performance can be assessed against data collected here. In total, twelve mechanisms were tested and presented in this work. All mechanisms need improvements at higher pressures for accurately predicting the measured IDTs. At lower pressures, some of the models agreed relatively well with the data. Some mechanisms predicted IDTs which were two orders of magnitudes different from the measurements. This suggests that there is behavior that has not been fully understood on the kinetic models and is inaccurate in predicting CO2 diluted environments for syngas combustion. To the best of our knowledge, current data are the first syngas IDTs measurements close to 50 atm under highly CO2 diluted (85% per vol.) conditions.
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      High-Pressure Oxy-Syngas Ignition Delay Times With CO2 Dilution: Shock Tube Measurements and Comparison of the Performance of Kinetic Mechanisms

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    contributor authorBarak, Samuel
    contributor authorNinnemann, Erik
    contributor authorNeupane, Sneha
    contributor authorBarnes, Frank
    contributor authorKapat, Jayanta
    contributor authorVasu, Subith
    date accessioned2019-03-17T09:53:03Z
    date available2019-03-17T09:53:03Z
    date copyright9/26/2018 12:00:00 AM
    date issued2019
    identifier issn0742-4795
    identifier othergtp_141_02_021011.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4255753
    description abstractIn this study, syngas combustion was investigated behind reflected shock waves in CO2 bath gas to measure ignition delay times (IDT) and to probe the effects of CO2 dilution. New syngas data were taken between pressures of 34.58–45.50 atm and temperatures of 1113–1275 K. This study provides experimental data for syngas combustion in CO2 diluted environments: ignition studies in a shock tube (59 data points in 10 datasets). In total, these mixtures covered a range of temperatures T, pressures P, equivalence ratios φ, H2/CO ratio θ, and CO2 diluent concentrations. Multiple syngas combustion mechanisms exist in the literature for modeling IDTs and their performance can be assessed against data collected here. In total, twelve mechanisms were tested and presented in this work. All mechanisms need improvements at higher pressures for accurately predicting the measured IDTs. At lower pressures, some of the models agreed relatively well with the data. Some mechanisms predicted IDTs which were two orders of magnitudes different from the measurements. This suggests that there is behavior that has not been fully understood on the kinetic models and is inaccurate in predicting CO2 diluted environments for syngas combustion. To the best of our knowledge, current data are the first syngas IDTs measurements close to 50 atm under highly CO2 diluted (85% per vol.) conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHigh-Pressure Oxy-Syngas Ignition Delay Times With CO2 Dilution: Shock Tube Measurements and Comparison of the Performance of Kinetic Mechanisms
    typeJournal Paper
    journal volume141
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4040904
    journal fristpage21011
    journal lastpage021011-7
    treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 002
    contenttypeFulltext
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