Transient phenomena during diffusion/edge flame transitions in an opposed-jet hydrogen/air burner

被引:12
作者
Frouzakis, CE [1 ]
Tomboulides, AG
Lee, J
Boulouchos, K
机构
[1] Paul Scherrer Inst, Combust Res Lab, CH-5232 Villigen, Switzerland
[2] ETHZ, Swiss Fed Inst Technol, IC Engines & Combust Technol Lab, CH-8092 Zurich, Switzerland
关键词
D O I
10.1016/S1540-7489(02)80194-8
中图分类号
O414.1 [热力学];
学科分类号
摘要
Time-accurate direct numerical simulations with detailed chemistry and transport were used to study transient effects during the transitions between different flame structures in an axisymmetric hydrogen/air opposed-jet burner. By starting from a steady flame and impulsively changing the flowrates, we simulated two different scenarios: (1) extinction of diffusion flames around the axis of symmetry and formation of a propagating edge flame that ultimately leads to a ring-shaped edge flame stabilizing away from the axis of symmetry, and (2) propagation of ring-shaped premixed flames along the stoichiometric isoline through a weakly stratified mixture in the direction normal to the direction of propagation, eventually closing the flame hole and re-establishing a disk-shaped diffusion flame. A front moving to quench or extend the diffusion flames is observed at the initial and final stages of cases 1 and 2, respectively. After extinction of or before re-establishment of the diffusion tail, the flames (as a whole) move in a quasi-steady manner with a propagating velocity relative to the fresh reactants that is close to the premixed laminar flame speed. No negatively propagating edge flame was found during extinction; before the transition to a strongly burning edge flame, the diffusion flame edge is convected outward with the local flow velocity. During re-ignition, the edge flame propagates all the way to the axis, and no homogeneous re-ignition was observed. Close to the axis it attains a propagation velocity that is almost twice the laminar flame speed.
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页码:1581 / 1587
页数:7
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