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Fig. 1. Experimental (symbols) and simulated (lines) laminar flame speed of A1 (JP-8) in air at 403 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 A1 (JP-8) in O₂ at an equivalence ratio of 0.9 (top panel) and 1.05 (bottom panel) 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, 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.