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

Table 1

Three experiment conditions.

Run (experiment)	𝜆	𝐴air (mm^2)	𝑉air (m/s)
1	1.5	114.8	66
2	2	114.8	88
3	2.4	114.8	108

For all conditions: atmospheric pressure; fuel thermal input = 8 kW, fuel inlet velocity = 17.7 m/s; air inlet temperature = 600 K; fuel inlet temperature = 300 K.