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

Table 4

CFD simulation conditions.

Run (CFD)	𝜆	𝐴air (mm^2)	𝑉air (m/s)
1	1.5	114.8	66
6^∗	1.5	88.3	86
7	1.5	71.7	106
8	1.5	42.9	176
9	1.5	153.1	66
10	1.5	187.8	66

∗By keeping excess air coefficient constant with nitrogen dilution.