Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation

<table class="table-group" id="tab3"><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 3)</td><td align="center">Computational time, 1st iteration</td><td align="center">Total computational time, 30 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">10074507</td><td align="center">5585758</td><td align="center">35 m and 30 s</td><td align="center">35 m and 34 s</td><td align="center">
                44.5%</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/#testcase2">2</a>.

Mathematical Problems in Engineering

tab3

Table 3

Table 3: Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation 