BACK TO LIST

Fig. 1. Experimental (symbols) and simulated (lines) extinction strain rate of non-premixed RP2-1/N₂ against O₂ with the RP2-1/N₂ jet temperature at 473 K and O₂ temperature at 300 K (right panel). 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.