Numerical Analysis of Turbulent Combustion in a Model Swirl Gas Turbine Combustor

Figure 9

Predicted time-averaged fields of (a) temperature URANS-SST, (b) CO mass fraction URANS-SST, (c) temperature URANS-RSM, and (d) temperature LES, in a plane through combustor.

(a)

(b)

(c)

(d)