Advances in Aerodynamics

Table 1 Operation conditions for the simulations

From: Numerical study on the combustion process in a gas turbine combustor with different reference velocities

	U_ref [m/s]	P [atm]	T_inlet [K]	FAR [-]
Case 1	25	6.5	540	0.018
Case 2	8	6.5	540	0.018

Back to article page