Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td align="left">Initial objective function</td><td align="center">Minimum objective function (iteration 34)</td><td align="center">Computational time, 1st iteration</td><td align="center">Total computational time, 100 iterations</td><td align="center">Percentage of reduction in objective function</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td align="left">898639</td><td align="center">368148</td><td align="center">9 m and 32 s</td><td align="center">9 m and 43 s</td><td align="center">59%</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Results for Test Case <a href="https://static.hindawi.com/articles/mpe/volume-2014/505372/figures/#testcase3">3</a>.

Mathematical Problems in Engineering

tab5

Table 5

Table 5: Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation 