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Fig. 1. Experimental (symbols) and computed (solid lines) time histories and yields of key species measured during shock tube pyrolysis of 0.8 % Shell D in argon. In panels (a) and (c), the dashed lines represent the ±15 K temperature sensitivity computed for the species mole fraction; in panels (b) and (d), the error bars represent ±15 K of temperature uncertainty and 2-standard deviation of the measured species concentrations, and the pressure values indicated are the mean pressures of the respective experiments. The experimental 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.