TY - JOUR
T1 - Burning velocity of triple flames with gentle concentration gradient
AU - Hirota, Mitsutomo
AU - Yokomori, Takeshi
AU - Yasuda, Kyouhei
AU - Nagai, Yoshitaka
AU - Mizomoto, Masahiko
AU - Masuya, Goro
N1 - Funding Information:
This research was supported by the Ministry of Education, Science, Sports and Culture, Grant-in-Aid for Young Scientists (B), 17760154, 2005.
PY - 2007
Y1 - 2007
N2 - We investigated the local flame speed of a two-dimensional, methane-air triple flame in a rectangular burner. The velocity fields and the concentration profiles were measured with particle image velocimetry and the Rayleigh scattering method, respectively. There was a requisite combination of initial velocity and initial concentration gradient for consistency of the local concentration gradient at the leading edge of the flame. In these cases, the flame curvatures were also consistent. Accordingly, the burning velocity, defined as local flow velocity at the triple point, was determined by the flame curvature. The burning velocity increased with increasing flame curvature, when the curvature was near zero. After that, the burning velocity decreased with increasing curvature. The peak value thus exceeded the adiabatic one-dimensional laminar burning velocity. Comparing the effects of the measured flame stretch rate on the flow strain κs and flame curvature κc, κs is larger and increases more rapidly than κc for flame curvatures satisfying 1/Rf < 250 m-1 and then becomes constant while κc still increases for 250 m-1 < 1/Rf, so that κc becomes much larger than κs. There is also a peak in burning velocity at roughly the transition in flame curvature specified above. Therefore, the burning velocity for a low concentration gradient correlates with the flame stretch rate.
AB - We investigated the local flame speed of a two-dimensional, methane-air triple flame in a rectangular burner. The velocity fields and the concentration profiles were measured with particle image velocimetry and the Rayleigh scattering method, respectively. There was a requisite combination of initial velocity and initial concentration gradient for consistency of the local concentration gradient at the leading edge of the flame. In these cases, the flame curvatures were also consistent. Accordingly, the burning velocity, defined as local flow velocity at the triple point, was determined by the flame curvature. The burning velocity increased with increasing flame curvature, when the curvature was near zero. After that, the burning velocity decreased with increasing curvature. The peak value thus exceeded the adiabatic one-dimensional laminar burning velocity. Comparing the effects of the measured flame stretch rate on the flow strain κs and flame curvature κc, κs is larger and increases more rapidly than κc for flame curvatures satisfying 1/Rf < 250 m-1 and then becomes constant while κc still increases for 250 m-1 < 1/Rf, so that κc becomes much larger than κs. There is also a peak in burning velocity at roughly the transition in flame curvature specified above. Therefore, the burning velocity for a low concentration gradient correlates with the flame stretch rate.
KW - Burning velocity
KW - Concentration gradient
KW - Flame curvature
KW - Flame stretch rate
KW - Triple flame
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U2 - 10.1016/j.proci.2006.08.068
DO - 10.1016/j.proci.2006.08.068
M3 - Conference article
AN - SCOPUS:34548715410
SN - 1540-7489
VL - 31 I
SP - 893
EP - 899
JO - Proceedings of the Combustion Institute
JF - Proceedings of the Combustion Institute
IS - 1
T2 - 31st International Symposium on Combustion
Y2 - 5 August 2006 through 11 August 2006
ER -