Simulation of Combustion

The figure at the link side shows the turbulent rate of reaction of a combustion process in a gas turbine combustor, directly after the fuel nozzle. The numerical calculations assume that a non-premixed fuel in a Lean Direct Injection (LDI) exits the fuel nozzle as a spray.

The figure at the bottom of the page shows the temperature distribution in the longitudinal cross-sectional plane of the combustor