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Fig. 1. Yields of C₂H₄ and CH₄ measured (symbols) and simulated (lines) from thermal decomposition of 0.76 % (mol) RP2-2 in Ar in shock tube at p₅ = 13.5 atm. The data are taken from [1].

 

Fig. 2. Selected time histories of C₂H₄ and CH₄ measured (symbols) and simulated (lines) from thermal decomposition of RP2-2 (POSF5433) in argon in the Stanford shock tube. The dotted lines are simulations bracketing the ±15 K temperature uncertainty. The 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.