Analysis of the Shock Wave/Boundary Layer Interaction considering a Compression Corner Model Using the MacCormack Method

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Domain size</td><td class="align_center">Iterations</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">50 × 50</td><td class="align_center">2594</td></tr><tr><td class="align_left">100 × 100</td><td class="align_center">5141</td></tr><tr><td class="align_left">150 × 150</td><td class="align_center">7548</td></tr><tr><td class="align_left">200 × 200</td><td class="align_center">9880</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Journal of Engineering

tab4

Table 4

Table 4: Analysis of the Shock Wave/Boundary Layer Interaction considering a Compression Corner Model Using the MacCormack Method 