Effect of Dual Fuel Nozzle Structures on Combustion Flow Field in CRGT Combustor

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="913837.fig.0010a" src="https://static.hindawi.com/articles/mpe/volume-2013/913837/figures/913837.fig.0010a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Inner swirl nozzle </td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="913837.fig.0010b" src="https://static.hindawi.com/articles/mpe/volume-2013/913837/figures/913837.fig.0010b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Double swirl nozzle  </td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="913837.fig.0010c" src="https://static.hindawi.com/articles/mpe/volume-2013/913837/figures/913837.fig.0010c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>Outer swirl nozzle</td></tr></table></td></tr></table>

<table>Temperature distributions in the combustor.</table>

Mathematical Problems in Engineering

fig10

Figure 10

Figure 10: Effect of Dual Fuel Nozzle Structures on Combustion Flow Field in CRGT Combustor 