TY - GEN
T1 - Experimental shock tube measurements of laminar burning velocity of n-heptane and iso-octane in the negative temperature coefficient regime
AU - Susa, Adam J.
AU - Ferris, Alison M.
AU - Davidson, David F.
AU - Hanson, Ronald K.
N1 - Publisher Copyright:
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - 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.
AB - 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.
UR - https://www.scopus.com/pages/publications/85083943878
UR - https://www.scopus.com/pages/publications/85083943878#tab=citedBy
U2 - 10.2514/6.2019-0460
DO - 10.2514/6.2019-0460
M3 - Conference contribution
AN - SCOPUS:85083943878
SN - 9781624105784
T3 - AIAA Scitech 2019 Forum
BT - AIAA Scitech 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2019
Y2 - 7 January 2019 through 11 January 2019
ER -