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

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td align="left">Hole shape</td><td align="center">Blowing ratio</td><td align="center">Maximum average overall film cooling effectiveness</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td align="left">LFDSA-00-00</td><td align="center">1.1</td><td align="center">0.174</td></tr><tr><td align="left">LFDSA-10-10</td><td align="center">4.0</td><td align="center">0.200</td></tr><tr><td align="left">LFDSA-15-15</td><td align="center">2.0</td><td align="center">0.240</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Average overall film cooling effectiveness at different blowing ratios.

International Journal of Aerospace Engineering

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Table 1

Table 1: Film Cooling Optimization Using Numerical Computation of the Compressible Viscous Flow Equations and Simplex Algorithm 