Fig. C.3
Mole fraction of methanol (top) and carbon monoxide (bottom) versus time for the combustion of methanol in a shock tube for a pressure around 2.5 atm, and an equivalence ratio of 1. The points represent experimental data from Ren et al. (2013), and the lines show modeling results using the chemical scheme of Venot et al. (2012) (dashed) and with the updated chemical scheme of this paper (solid). P = 2.2 atm, (right) P = 1.1 atm.
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