Film Cooling Optimization Using Numerical Computation of the Compressible Viscous Flow Equations and Simplex Algorithm

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="859465.fig.0022a" src="https://static.hindawi.com/articles/ijae/volume-2013/859465/figures/859465.fig.0022a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Coolant velocity normal to boundary</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="859465.fig.0022b" src="https://static.hindawi.com/articles/ijae/volume-2013/859465/figures/859465.fig.0022b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Coolant velocity in direction of streamwise angle</td></tr></table></td></tr></table>

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International Journal of Aerospace Engineering

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Figure 22

Figure 22: Film Cooling Optimization Using Numerical Computation of the Compressible Viscous Flow Equations and Simplex Algorithm 