Combust. Flame (2016)

Effects of non-unity Lewis number of gas-phase species in turbulent nonpremixed

A Attili, F Bisetti, M E Mueller, and H Pitsch. “Effects of non-unity Lewis number of gas- phase species in turbulent nonpremixed”. Combust. Flame 1 (2016). In press.

A Attili, F Bisetti, M E Mueller, H Pitsch
Flames, differential diffusion,
2016
​Turbulence statistics from two different three-dimensional direct numerical simulations of planar n-heptane/air turbulent jets are compared to assess the effect of the gas-phase species diffusion model on flame dynamics and soot formation. The Reynolds number based on the initial jet width and velocity is around 15000, corresponding to a Taylor scale Reynolds number in the range 100 ≤ Reλ ≤ 150. In one simulation, multicomponent transport based on a mixture-averaged approach is employed, while, in the other, the gas-phase species Lewis numbers are set equal to unity. The statistics of temperature and major species obtained with the mixture-averaged formulation are very similar to those in the unity Lewis number case. In both cases, the statistics of temperature are captured with remarkable accuracy by a laminar flamelet model with unity Lewis numbers. On the contrary, a flamelet model with a mixture-averaged diffusion model, which correspond to that used in the multi-component diffusion three-dimensional DNS, produces significant differences with respect to the DNS results. The total mass of soot precursors decreases by 20 to 30% with the unity Lewis number approximation, and their distribution is more homogeneous in space and time. Due to the non-linearity of the soot growth rate with respect to the precursors’ concentration, the soot mass yield decreases by a factor of two. Being strongly affected by coagulation, soot number density is not altered significantly if the unity Lewis number model is used rather than the mixture-averaged diffusion. These observations that turbulent transport in part or completely overshadows differential diffusion effects is expected to become more pronounced for higher Reynolds numbers.​