Established Numerical Techniques for the Structural Analysis of a Regional Aircraft Landing Gear

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left" colspan="2">Material properties</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Wheel axle</td><td class="align_center">300M AMS6257</td></tr><tr><td class="align_left">Main fitting/trailing arm</td><td class="align_center">AL7175-T74 AMS 4149</td></tr><tr><td class="align_left">Folding side brace</td><td class="align_center">Ti6Al4V AMS4928</td></tr><tr><td class="align_left">Shock absorber cylinder</td><td class="align_center">4340 AMS 6414</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Advances in Materials Science and Engineering

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Table 1

Table 1: Established Numerical Techniques for the Structural Analysis of a Regional Aircraft Landing Gear 