Experimental and numerical studies were conducted to grasp the flame characteristics for mutually interacting SNG-air premixed flames with a counterflow configuration. Five different reaction mechanisms (GRI 3.0, USC 2.0, Aramco 2.0, UCSD, and CRECK) were tested to give the priority in tracing measured lean extinction boundaries. UCSD mechanism best traced the measured data. The flame stability map was presented with a functional dependency on methane mole fractions in the reactant streams issuing from the lower and upper nozzles, by varying the global strain rate.With increasing global strain rate, lean and rich extinction boundaries were gradually slanted, forming an island of flammable region and finally only one flammable condition at 740 s−1 via a continuous shrinkage of flammable region. For asymmetric lean-lean and rich-rich flames, the weaker flame was survived via thermally and chemically symbiotic relation of it to the stronger flame. For lean-rich flames, triple flame is changed into bi-brachial flames via a merging of diffusion flame lean flame at high strain rates. This behavior could be explained well by introducing a specific heat release rate. Extinction mechanism could be reasonably explained by the relation of specific heat release rate (as a reactivity of flame) to conductive heat loss from the strong flame to unburned mixture.
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