Combustion control strategies to minimize the pollutants emission from
municipal solid waste (MSW) incinerators are formulated based on the
improved mixing of air with the products of incomplete combustion and
the subsequent increase in oxidative destruction. Secondary air inject
ion into the combustion chamber plays the key role in this mixing proc
ess. However, design variables of the air jet into the combustion gas
stream are not clearly identified, and the performance of mixing and r
eaction is not fully understood. Three-dimensional flow simulation was
performed to study the mixing performance of a full-scale incinerator
combustion chamber according to the secondary air nozzle configuratio
n. A detailed flow was analyzed and the degree of mixing was quantitat
ively evaluated by introducing a statistical parameter based on the ch
emical species distribution. The gas residence time distribution was a
nalyzed using the particle trajectory. The overall how held was strong
ly influenced by the nozzle configuration. It was demonstrated that th
e degree of mixing could be improved by selecting larger inter-jet spa
cing and stronger jet velocity. The staggered arrangement of two oppos
ite nozzle arrays was found to be more effective in terms of mixing an
d gas residence time distribution.