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Fig. 1. Experimental (symbols) and simulated (lines) laminar flame speed of Shell D in air at 373 K unburned gas temperature and 1 atm pressure. The error bars represent ±2σ data uncertainties. Data are taken from [1].

Fig. 2. Experimental (symbols) and simulated (lines) laminar flame speed of Shell D in O₂ at an equivalence ratio of 1.003 with N₂ and He as the diluent gas at elevated pressures. The temperature values given in the plots are the unburned gas temperatures at the corresponding pressures. The error bars represent ±2σ data uncertainties. Data are taken from [1].

Reference

[1]  R. Xu, C. Saggese, R. Lawson, A. Movaghar, T. Parise, J.Shao, R. Choudhary, J. Park, T. Lu, R.K. Hanson, D.F. Davidson, F.N. Egolfopoulos, A. Aradi, A. Prakash, V.R.R. Mohan, R. Cracknell, H. Wang, A physics-based approach to modeling real-fuel combustion chemistry - VI. Predictive kinetic models of gasoline fuels, Combustion and Flame 220 (2020) 475-487.