I'm trying to simulate pulsejet engine combustion using a matlab code, but i'm stuck at the combustion phase.

1) I should use "G. PACZKO, P.M. LEFDAL AND N. PETERS" mechanism mentioned in (REDUCED REACTION SCHEMES FOR METHANE, METHANOL AND PROPANE FLAMES), the problem here is i don't know how to implement a reduced chemical kinetic mechanism using the paper's definitions (global reaction rate and how to relate it to the molar concentrations of the species variation with time) ?

2) How do i implement that chemical mechanism in NS equations ? when to call it, what does it need as inputs, what will it give me as outputs, .. etc.

Any help would be so appreciated.

Thanks all

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