Fuel-rich n-heptane oxidation: A shock tube and laser absorption study

Zachary E. Loparo, Joseph G. Lopez, Sneha Neupane, William P. Partridge, Konstantin Vodopyanov, Subith S. Vasu

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Abstract

The chemical kinetics of n-heptane (n-C7H16) – an important reference compound for real fuels – oxidation are well studied at stoichiometric and lean conditions. However, there is only limited information on the n-heptane chemical kinetics in fuel-rich combustion. In order to verify the accuracy of chemical kinetic models at these conditions, the oxidation of rich n-heptane mixtures has been investigated. Combustion of n-C7H16/O2/Ar mixtures at equivalence ratios, φ, of 2.0 and 3.0 behind reflected shock waves has been studied at temperatures ranging from 1066 to 1502 K and at pressures ranging from 1.4 to 6.2 atm. Reaction progress was monitored by recording pressure and absorption time-histories of ethylene (C2H4) and n-heptane at a location 2 cm from the endwall of a 14-cm inner diameter shock tube. Ethylene and n-heptane absorption time-histories were measured, respectively, using absorption spectroscopy at 10.532 μm from a tunable CO2 laser and at around 3.4 μm from a continuous wave distributed feedback interband cascade laser (ICL). The measured absorption time-histories were compared with modeled predictions from the Lawrence Livermore National Lab (LLNL) detailed n-heptane reaction mechanism. To the best of our knowledge, current data are the first time-resolved n-heptane and ethylene concentration measurements conducted in a shock tube at these conditions.

Original languageEnglish
Pages (from-to)220-233
Number of pages14
JournalCombustion and Flame
Volume185
DOIs
StatePublished - 2017

Funding

This material is based upon work supported by the National Science Foundation Graduate Research Fellowship Program under Grant no. 1144246. Donors of the American Chemical Society Petroleum Research Fund and the Defense Threat Reduction Agency (Grant number: HDTRA1-16-1-0009) are acknowledged for partial financial support. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the author(s) and do not necessarily reflect the views of the National Science Foundation. J.L. acknowledges funding provided by the National Aeronautics and Space Administration Florida Space Grant Consortium. The authors thank assistance from Owen Pryor, Leigh Nash, and Sam Barak during UCF shock tube experiments. The Oak Ridge National Laboratory research was sponsored by the U.S. Department of Energy, Office of Energy Efficiency and Renewable Energy, Vehicle Technologies Office, with Gurpreet Singh as the Program Managers.

FundersFunder number
National Aeronautics and Space Administration Florida Space Grant Consortium
Office of Energy Efficiency and Renewable Energy, Vehicle Technologies Office
National Science Foundation
U.S. Department of Energy
Directorate for Education and Human Resources1144246
Defense Threat Reduction AgencyHDTRA1-16-1-0009
American Chemical Society Petroleum Research Fund

    Keywords

    • Chemical kinetics
    • Fuel rich
    • Laser absorption
    • Shock tube
    • n-Heptane

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