Fig. 1. Measured (closed symbols) and simulated (open symbols) species yields from thermal decomposition of 0.63% A2 in argon at a nominal pressure of p₅ = 12.4 atm in the UIC single-pulse shock tube. The dwell time ranges from 1.85 to 2.39 ms. Error bars represent temperature uncertainty determined from shock velocity and experimental uncertainties of the species concentrations. 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.