TY - JOUR
T1 - Flame acceleration in channels with obstacles in the deflagration-to-detonation transition
AU - Valiev, Damir
AU - Bychkov, Vitaly
AU - Akkerman, V'yacheslav
AU - Law, Chung King
AU - Eriksson, Lars Erik
N1 - Funding Information:
This work was mostly supported by the Swedish Research Council (VR) and the Swedish Kempe Foundation. The numerical simulation was performed at the High Performance Computer Center North (HPC2N), Umea, Sweden, under SNAC Project 007-07-25. The work at Princeton University was supported by the US Air Force Office of Scientific Research.
PY - 2010/5
Y1 - 2010/5
N2 - It was demonstrated recently in Bychkov et al. [Bychkov et al., Phys. Rev. Lett. 101 (2008) 164501], that the physical mechanism of flame acceleration in channels with obstacles is qualitatively different from the classical Shelkin mechanism. The new mechanism is much stronger, and is independent of the Reynolds number. The present study provides details of the theory and numerical modeling of the flame acceleration. It is shown theoretically and computationally that flame acceleration progresses noticeably faster in the axisymmetric cylindrical geometry as compared to the planar one, and that the acceleration rate reduces with increasing Mach number and thereby the gas compressibility. Furthermore, the velocity of the accelerating flame saturates to a constant value that is supersonic with respect to the wall. The saturation state can be correlated to the Chapman-Jouguet deflagration as well as the fast flames observed in experiments. The possibility of transition from deflagration-to-detonation in the obstructed channels is demonstrated.
AB - It was demonstrated recently in Bychkov et al. [Bychkov et al., Phys. Rev. Lett. 101 (2008) 164501], that the physical mechanism of flame acceleration in channels with obstacles is qualitatively different from the classical Shelkin mechanism. The new mechanism is much stronger, and is independent of the Reynolds number. The present study provides details of the theory and numerical modeling of the flame acceleration. It is shown theoretically and computationally that flame acceleration progresses noticeably faster in the axisymmetric cylindrical geometry as compared to the planar one, and that the acceleration rate reduces with increasing Mach number and thereby the gas compressibility. Furthermore, the velocity of the accelerating flame saturates to a constant value that is supersonic with respect to the wall. The saturation state can be correlated to the Chapman-Jouguet deflagration as well as the fast flames observed in experiments. The possibility of transition from deflagration-to-detonation in the obstructed channels is demonstrated.
KW - Deflagration-to-detonation transition
KW - Flame acceleration
KW - Flame-obstacle interaction
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U2 - 10.1016/j.combustflame.2009.12.021
DO - 10.1016/j.combustflame.2009.12.021
M3 - Article
AN - SCOPUS:77349116812
SN - 0010-2180
VL - 157
SP - 1012
EP - 1021
JO - Combustion and Flame
JF - Combustion and Flame
IS - 5
ER -