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The effects of chemical kinetic mechanisms on large eddy simulation (LES) of a nonpremixed hydrogen jet flame

机译:化学动力学机理对非预混合氢射流火焰大涡模拟(LES)的影响

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摘要

Five different chemical mechanisms for hydrogen combustion are employed in large eddy simulation of a nonpremixed hydrogen jet flame to investigate the ability of these mechanisms to represent the turbulence-chemistry interactions and other combustion phenomena. The mechanisms studied include a reduced mechanism, two detailed H2/O2 reaction mechanisms, as well as a detailed H2/CO mechanism and the GRI3.0 mechanism. Linear eddy model is incorporated to evaluate the effect of turbulence-chemistry interactions. Extensive simulations of a well-known experimental case (German Aerospace Centre DLR nonpremixed flame M2) have been performed for the purpose of validation. Comparisons against experimental data including scalar distribution profiles are presented where a reasonable agreement is observed for the detailed mechanisms. Flux analyses of the species conservation equations and ignition delay time tests showed that chemical kinetics plays a role in the development of flame structures in the jet flame. This study highlights the importance of precise descriptions of the chemical kinetics in LES of nonpremixed hydrogen combustion.
机译:在未预混合氢射流火焰的大涡模拟中,采用了五种不同的氢燃烧化学机理来研究这些机理代表湍流-化学相互作用和其他燃烧现象的能力。研究的机理包括还原机理,两个详细的H2 / O2反应机理,详细的H2 / CO机理和GRI3.0机理。线性涡流模型被纳入评估湍流-化学相互作用的影响。为了进行验证,对众所周知的实验案例(德国航空航天中心DLR非预混火焰M2)进行了广泛的模拟。提出了与包括标量分布曲线在内的实验数据的比较,其中对详细的机理观察到合理的一致性。对物种守恒方程的通量分析和点火延迟时间测试表明,化学动力学在喷射火焰中的火焰结构发展中起作用。这项研究突显了精确描述非预混合氢燃烧LES中化学动力学的重要性。

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