Experimental shock tube measurements of laminar burning velocity of n-heptane and iso-octane in the negative temperature coefficient regime

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Laminar burning velocities (SL) of n-heptane and iso-octane are measured between 400 and 900 K at 1 atm and 0.9 equivalence ratio. A shock tube is used to heat the unburned gas to temperatures at which it would auto-ignite, while limiting the time for ignition chemistry to occur ahead of the flame to much less than the ignition delay time. In air (21% O2, 79% N2), measured values of SL are lower than, but follow the same temperature trend as the model below 550 K; between 550 and 600 K, a stronger dependence of SL on temperature is observed. For SL measurements performed in a helium-containing oxidizer (18% O2, 41% N2, 41% He), a strong temperature dependence, similar to that seen in air, is observed between 600 and 700 K. Between 700 and 800 K, a negative temperature dependence is observed. Above 800 K, measured SL again assumes a positive temperature dependence. While negative temperature coefficient (NTC) behavior is known to exist in ignition delay times for many hydrocarbon fuels, to the authors’ knowledge, this work represents the first direct, experimental observation of NTC behavior in flame speed measurements.

Original languageEnglish (US)
Title of host publicationAIAA Scitech 2019 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105784
DOIs
StatePublished - 2019
Externally publishedYes
EventAIAA Scitech Forum, 2019 - San Diego, United States
Duration: Jan 7 2019Jan 11 2019

Publication series

NameAIAA Scitech 2019 Forum

Conference

ConferenceAIAA Scitech Forum, 2019
Country/TerritoryUnited States
CitySan Diego
Period1/7/191/11/19

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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