Laminar-flame instabilities in a taylor-couette combustor
Laminar-flame instabilities in a taylor-couette combustor
复制标题
泰勒库埃特燃烧器中的层流火焰不稳定性
DOI:
10.1016/s0010-2180(99)00145-5
复制
发表时间:
2000
影响因子:
4.4
通讯作者:
R. Aldredge
中科院分区:
文献类型:
--
作者:
V. Vaezi;R. Aldredge
Premixed-flame propagation in a Taylor-Couette combustor has been studied experimentally in order to examine the influence of laminar-flame instabilities on the burning velocity and flow-field properties upstream of the flame. An initially wrinkled annular flame propagating downward, away from the open end of the combustor, is found to undergo first deceleration and planarization and then acceleration and enhanced surface wrinkling, while intensities of axial and circumferential velocity fluctuations upstream of the flame, initially negligible, are strongly amplified. The evolution of flame speeds recorded during propagation in lean and stoichiometric methane–air mixtures is in good qualitative agreement with that found in earlier experiments of downward propane–air flame propagation in tubes. It is determined that primary and secondary laminar-flame instabilities associated with the coupling between acoustic waves and the rate of chemical heat release govern the evolution of both the flame-speed and the upstream flow field in the TC combustor, as was found in earlier experiments and predicted theoretically for downward flame propagation in tubes. The results are the first to describe laminar-flame instabilities in a TC combustor and to identify the development and growth of transverse acoustic waves associated with the secondary acoustic instability.