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.007a" src="https://static.hindawi.com/articles/mpe/volume-2013/913837/figures/913837.fig.007a.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.007b" src="https://static.hindawi.com/articles/mpe/volume-2013/913837/figures/913837.fig.007b.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.007c" src="https://static.hindawi.com/articles/mpe/volume-2013/913837/figures/913837.fig.007c.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>Streamlines of velocity field for different dual fuel nozzle structures.</table>

Mathematical Problems in Engineering

fig7

Figure 7

Figure 7: Effect of Dual Fuel Nozzle Structures on Combustion Flow Field in CRGT Combustor 