Combustion Turbulence Flow in the Advanced Vortex Combustor with Built-In Obstacles

Table 3

Specification of calculation conditions.

Equivalence ratio	0.4, 0.6, 0.8, 1.0, 1.2, 1.4
Inlet velocity /(m/s)	10, 30, 50, 70, 90, 110
Inlet temperature /K	300, 400, 500, 600, 700