Numerical Simulation of Air Inlet Conditions Influence on the Establishment of MILD Combustion in Stagnation Point Reverse Flow Combustor

<table>Comparison the predicted and measured temperature, CO<sub>2</sub> and O<sub>2</sub> mole fraction [<a href="/journals/mpe/2013/593601/#B11">10</a>].</table>

Mathematical Problems in Engineering

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Figure 2

Figure 2: Numerical Simulation of Air Inlet Conditions Influence on the Establishment of MILD Combustion in Stagnation Point Reverse Flow Combustor 