Web Optimization of Compression Ignition Aviation Engine Crankshaft

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Mesh metric</td><td class="align_center">PSE</td><td class="align_center">Min value</td><td class="align_center">Max value</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Aspect ratio</td><td class="align_center">1.0</td><td class="align_center">1.0</td><td class="align_center">3.0</td></tr><tr><td class="align_left">Jacobian ratio</td><td class="align_center">1.0</td><td class="align_center">0.7</td><td class="align_center">1.0</td></tr><tr><td class="align_left">Element quality</td><td class="align_center">1.0</td><td class="align_center">0.7</td><td class="align_center">1.0</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: Web Optimization of Compression Ignition Aviation Engine Crankshaft 