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

Table 2

Characteristic parameters of combustion.

Run	Peak temperature	𝑅tu	𝑅eg
1	1870.6 K	8.03%	70.9%
2	1530.8 K	4.87%	82.7%
3	1426.9 K	3.65%	90.7%