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

Figure 7

Predicted time-averaged velocity fields in a plane through combustor for NG-FGR20 flame: (a) axial velocity URANS-SST, (b) velocity magnitude URANS-SST, (c) axial velocity URANS-RSM, and (d) axial velocity LES.

(a)

(b)

(c)

(d)