Time-resolved measurements of intermediate concentrations in fuel-rich N-heptane oxidation behind reflected shock waves

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

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

5 Scopus citations

Abstract

The chemical kinetics of the oxidation of n-heptane (C7H16) - an important reference compound for real fuels - are well studied at stoichiometric and lean conditions. However, there is only limited information on the chemical kinetics of fuel-rich combustion. In order to improve the accuracy of chemical kinetic models at these conditions, the oxidation of rich nheptane mixtures has been investigated. Combustion of n-C7H16/O2/Ar mixtures at equivalence ratios, φ, of 2.0 behind reflected shock waves has been studied at temperatures ranging from 1075 to 1418K and at pressures ranging from 1.6 to 1.9atm. Reaction progress was monitored by recording ethylene (C2H4) concentration time-histories and initial n-heptane decay rates at a location 2cm from the endwall of a 13.4m long, 14cm inner diameter shock tube. Ethylene and n-heptane concentration time-histories were measured using absorption spectroscopy at 10.532μm from a tunable CO2 laser and at around 3.4μm from a continuous wave distributed feedback interband cascade laser (ICL), respectively. The measured concentration 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, the current data are the first time-resolved nheptane and ethylene concentration measurements conducted in a shock tube at these conditions.

Original languageEnglish
Title of host publicationCombustion, Fuels and Emissions
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791850848
DOIs
StatePublished - 2017
EventASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, GT 2017 - Charlotte, United States
Duration: Jun 26 2017Jun 30 2017

Publication series

NameProceedings of the ASME Turbo Expo
Volume4A-2017

Conference

ConferenceASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, GT 2017
Country/TerritoryUnited States
CityCharlotte
Period06/26/1706/30/17

Funding

This material is based upon work supported by the National Science Foundation Graduate Research Fellowship Program under Grant No. 1144246. 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. 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. 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 Manager.

FundersFunder number
National Science Foundation1144246
U.S. Department of Energy
National Aeronautics and Space Administration
Defense Threat Reduction AgencyHDTRA1-16-1-0009
Office of Energy Efficiency and Renewable Energy
American Chemical Society Petroleum Research Fund

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