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Fig. 1. Selected time histories of C₂H₄ and CH₄ measured (symbols) and simulated (lines) from thermal decomposition of A1, A2, and A3 fuel in argon in the Stanford shock tube. The dotted lines are simulations bracketing the ±15 K temperature uncertainty. The data are taken from [1] and [2].

Reference

[1]  H. Wang, R. Xu, K. Wang, C.T. Bowman, D.F. Davidson, R.K. Hanson, K. Brezinsky, F.N. Egolfopoulos, A physics-based approach to modeling real-fuel combustion chemistry - I. Evidence from experiments, and thermodynamic, chemical kinetic and statistical considerations, Combustion and Flame 193 (2018) 502-519.

[2]  R. Xu, K. Wang, S. Banerjee, J. Shao, T. Parise, Y. Zhu, S. Wang, A. Movaghar, D.J. Lee, R. Zhao, X. Han, Y. Gao, T. Lu, K. Brezinsky, F.N. Egolfopoulos, D.F. Davidson, R.K. Hanson, C.T. Bowman, H. Wang, A physics-based approach to modeling real-fuel combustion chemistry - II. Reaction kinetic models of jet and rocket fuels, Combustion and Flame 193 (2018) 520-537.