Effect of Secondary Flows on Heat Transfer of a Gas Turbine Blade

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="797841.fig.0010a" src="https://static.hindawi.com/articles/ijrm/volume-2013/797841/figures/797841.fig.0010a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Pressure side</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="797841.fig.0010b" src="https://static.hindawi.com/articles/ijrm/volume-2013/797841/figures/797841.fig.0010b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Suction side</td></tr></table></td></tr></table>

<table>Surface Nusselt number, Re = 106000.</table>

International Journal of Rotating Machinery

fig10

Figure 10

Figure 10: Effect of Secondary Flows on Heat Transfer of a Gas Turbine Blade 