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NUMERICAL STUDY OF FLAME/VORTEX INTERACTIONS IN 2-D TRAPPED VORTEX COMBUSTOR

机译:二维捕集式涡流燃烧器火焰/涡流相互作用的数值研究

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摘要

The interactions between flame and vortex in a 2-D Trapped Vortex Combustor are investigated by simulating the Reynolds Averaged Navier Stokes (RANS) equations, for the following five cases namely (i) non-reacting (base) case, (ii) post-vortex ignition without premixing, (iii) post-vortex ignition with premixing, (iv) pre-vortex ignition without premixing and (v) pre-vortex ignition with premixing. For the post-vortex ignition without premixing case, the reactants are mixed well in the cavity resulting in a stable ‘C’ shaped flame along the vortex edge. Further, there is insignificant change in the vorticity due to chemical reactions. In contrast, for the pre-vortex ignition case (no premixing); the flame gets stabilized at the interface of two counter rotating vortices resulting in reduced reaction rates. There is a noticeable change in the location and size of the primary vortex as compared to case (ii). When the mainstream air is premixed with fuel, there is a further reduction in the reaction rates and thus structure of cavity flame gets altered significantly for case (v). Pilot flame established for cases (ii) and (iii) are well shielded from main flow and hence the flame structure and reaction rates do not change appreciably. Hence, it is expected that cases (ii) and (iii) can perform well over a wide range of operating conditions.
机译:通过模拟雷诺兹平均Navier斯托克斯(RANS)方程,研究了以下两种情况,即(i)非反应(基础)情况,(ii)后处理,二维陷井涡流燃烧器中火焰与涡旋之间的相互作用。不进行预混合的涡旋点火,(iii)不进行预混合的涡旋点火,(iv)不进行预混合的涡旋点火,以及(v)经过预混合的涡旋点火。对于没有预混合情况的涡流后点火,反应物在空腔中充分混合,沿涡流边缘形成稳定的“ C”形火焰。此外,由于化学反应,涡度的变化很小。相反,对于涡旋前点火情况(无预混合);火焰在两个反向旋转的涡旋的界面处稳定下来,导致反应速率降低。与情况(ii)相比,一次涡旋的位置和大小有明显变化。当主流空气与燃料预混合时,反应速率会进一步降低,因此对于情况(v),型腔火焰的结构会发生显着变化。为情况(ii)和(iii)建立的引燃火焰被很好地屏蔽了主流,因此火焰的结构和反应速率没有明显变化。因此,预计情况(ii)和(iii)可以在很宽的工作条件范围内很好地执行。

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