TY - JOUR
T1 - Heat Flux from Turbulent Premixed Flame to the Wall of a Constant Volume Vessel
AU - Tomita, Eiji
AU - Hamamoto, Yoshisuke
AU - Sasaki, Hiroshi
N1 - Copyright:
Copyright 2016 Elsevier B.V., All rights reserved.
PY - 1989
Y1 - 1989
N2 - Instantaneous heat flux to the wall of a combustion chamber was measured by a co-axial thermocouple with a thin fin junction for the case with laminar and turbulent flame of a propane-air mixture. The experiment was performed in a constant volume vessel of the disk-type with swirl flow. When the laminar flame arrived at the wall, the heat flux had one sharp peak. In the case of the turbulent flame, however, the heat flux with multiple sharp peaks was observed. It is considered that this phenomenon corresponds to the structure of the turbulent flame. The maximum value of peak heat flux, qmax is approximately proportional to {k(Ti-Tu)/δL}0.61, where (Ti-Tu)/δL is a characteristic value of the temperature gradient in a preheat zone of laminar flame and k is the heat conductivity. The same relation is obtained, even when the flow velocity, equivalence ratio or measuring position are varied.
AB - Instantaneous heat flux to the wall of a combustion chamber was measured by a co-axial thermocouple with a thin fin junction for the case with laminar and turbulent flame of a propane-air mixture. The experiment was performed in a constant volume vessel of the disk-type with swirl flow. When the laminar flame arrived at the wall, the heat flux had one sharp peak. In the case of the turbulent flame, however, the heat flux with multiple sharp peaks was observed. It is considered that this phenomenon corresponds to the structure of the turbulent flame. The maximum value of peak heat flux, qmax is approximately proportional to {k(Ti-Tu)/δL}0.61, where (Ti-Tu)/δL is a characteristic value of the temperature gradient in a preheat zone of laminar flame and k is the heat conductivity. The same relation is obtained, even when the flow velocity, equivalence ratio or measuring position are varied.
KW - Combustion
KW - Heat Flux
KW - Internal Combustion Engine
KW - Laminar Flame
KW - Turbulent Flame
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U2 - 10.1299/kikaib.55.1229
DO - 10.1299/kikaib.55.1229
M3 - Article
AN - SCOPUS:0024648218
SN - 0387-5016
VL - 55
SP - 1229
EP - 1233
JO - Transactions of the Japan Society of Mechanical Engineers Series B
JF - Transactions of the Japan Society of Mechanical Engineers Series B
IS - 512
ER -