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

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td align="left">Constituents</td><td align="center">CO</td><td align="center">CO<sub>2</sub></td><td align="center">H<sub>2</sub></td><td align="center">H<sub>2</sub>O</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td align="left">Mole fraction</td><td align="center">0.0561</td><td align="center">0.09979</td><td align="center">0.40208</td><td align="center">0.44203</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mathematical Problems in Engineering

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Table 1

Table 1: Effect of Dual Fuel Nozzle Structures on Combustion Flow Field in CRGT Combustor 