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Numerical analyses of deflagration initiation by a hot jet

机译:热喷射爆燃引发的数值分析

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摘要

Numerical simulations of axisymmetric reactive jets with one-step Arrhenius kineticsare used to investigate the problem of deflagration initiation in a premixed fuel–airmixture by the sudden discharge of a hot jet of its adiabatic reaction products. For themoderately large values of the jet Reynolds number considered in the computations,chemical reaction is seen to occur initially in the thin mixing layer that separates the hotproducts from the cold reactants. This mixing layer is wrapped around by the startingvortex, thereby enhancingmixing at the jet head, which is followed by an annular mixinglayer that trails behind, connecting the leading vortex with the orifice rim. A successfuldeflagration is seen to develop for values of the orifice radius larger than a criticalvalue aϲ in the order of the flame thickness of the planar deflagration δL. Introductionof appropriate scales provides the dimensionless formulation of the problem, withflame initiation characterised in terms of a critical Damk¨ohler number ∆ϲ = (aϲ/δL)²,whose parametric dependence is investigated. The numerical computations reveal that,while the jet Reynolds number exerts a limited influence on the criticality conditions,the effect of the reactant diffusivity on ignition is much more pronounced, with thevalue of ∆ϲ increasing significantly with increasing Lewis numbers Le. The reactantdiffusivity affects also the way ignition takes place, so that for reactants with Le ≳ 1 theflame develops as a result of ignition in the annular mixing layer surrounding the developingjet stem, whereas for highly diffusive reactants with Lewis numbers sufficientlysmaller than unity combustion is initiated in the mixed core formed around the startingvortex. The analysis provides increased understanding of deflagration initiation processes,including the effects of differential diffusion, and points to the need for furtherinvestigations incorporating detailed chemistry models for specific fuel–air mixtures.
机译:用一步法Arrhenius动力学进行轴对称反应射流的数值模拟,以研究通过绝热反应产物的热射流的突然排放而在预混合燃料-空气混合物中引发爆燃的问题。对于计算中考虑到的雷诺数适中的较大值,可以看到化学反应最初发生在将热产物与冷反应物分开的薄混合层中。该混合层被起始涡流包裹,从而增强了喷射头处的混合,随后是一个环形混合层,该混合层向后延伸,将前部涡流与孔口边缘连接起来。对于大于临界值a 1的孔半径的值,按照平面爆燃δL的火焰厚度的顺序,可以看到成功爆燃。适当尺度的引入提供了问题的无量纲表述,火焰起爆以临界达姆霍勒数Δϲ =(aϲ /δL)²为特征,并研究了其参数依赖性。数值计算表明,虽然雷诺数对临界条件的影响有限,但反应物扩散率对着火的影响更为明显,ΔLewis值随刘易斯数Le的增加而显着增加。反应物的扩散性还影响着火的发生方式,因此,对于Le≥1的反应物,在围绕着显影射流杆的环形混合层中着火会产生火焰,而对于高度扩散的刘易斯数小于整体燃烧的反应物,则在燃烧开始。混合核形成于起始涡周围。该分析提供了对爆燃引发过程(包括差异扩散的影响)的更多理解,并指出有必要进行进一步研究,以纳入针对特定燃料-空气混合物的详细化学模型。

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