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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February 2019
Research-Article
High-Pressure Oxy-Syngas Ignition Delay Times With CO2 Dilution: Shock Tube Measurements and Comparison of the Performance of Kinetic Mechanisms
Samuel Barak,
Samuel Barak
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
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Erik Ninnemann,
Erik Ninnemann
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
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Sneha Neupane,
Sneha Neupane
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
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Frank Barnes,
Frank Barnes
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
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Jayanta Kapat,
Jayanta Kapat
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
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Subith Vasu
Subith Vasu
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
e-mail: subith@ucf.edu
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
e-mail: subith@ucf.edu
Search for other works by this author on:
Samuel Barak
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Erik Ninnemann
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Sneha Neupane
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Frank Barnes
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Jayanta Kapat
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
Subith Vasu
Center for Advanced Turbomachinery and
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
e-mail: subith@ucf.edu
Energy Research (CATER),
Mechanical and Aerospace Engineering,
University of Central Florida,
Orlando, FL 32816
e-mail: subith@ucf.edu
Manuscript received July 3, 2018; final manuscript received July 8, 2018; published online September 26, 2018. Editor: Jerzy T. Sawicki.
J. Eng. Gas Turbines Power. Feb 2019, 141(2): 021011 (7 pages)
Published Online: September 26, 2018
Article history
Received:
July 3, 2018
Revised:
July 8, 2018
Citation
Barak, S., Ninnemann, E., Neupane, S., Barnes, F., Kapat, J., and Vasu, S. (September 26, 2018). "High-Pressure Oxy-Syngas Ignition Delay Times With CO2 Dilution: Shock Tube Measurements and Comparison of the Performance of Kinetic Mechanisms." ASME. J. Eng. Gas Turbines Power. February 2019; 141(2): 021011. https://doi.org/10.1115/1.4040904
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