Vibration Reduction Design and Test of UAV Load Radar

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td class="align_left">Component</td><td class="align_center">Gasket</td><td class="align_center">Sleeve</td><td class="align_center">Retaining ring</td><td class="align_center">Rubber</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td class="align_left">Material</td><td class="align_center">Q235</td><td class="align_center">Q235</td><td class="align_center">Q235</td><td class="align_center">ZN-37</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

tab2

Table 2

Table 2: Vibration Reduction Design and Test of UAV Load Radar 