Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Symbol</td><td class="align_center">Values</td><td class="align_center">Unit</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Exx</td><td class="align_center">0.0354</td><td class="align_center">MPa</td></tr><tr><td class="align_left">Eyy</td><td class="align_center">0.0354</td><td class="align_center">MPa</td></tr><tr><td class="align_left">Ezz</td><td class="align_center">655.87</td><td class="align_center">MPa</td></tr><tr><td class="align_left">Gxy</td><td class="align_center">0.0266</td><td class="align_center">MPa</td></tr><tr><td class="align_left">Gyz</td><td class="align_center">141.12</td><td class="align_center">MPa</td></tr><tr><td class="align_left">Gzx</td><td class="align_center">92.463</td><td class="align_center">MPa</td></tr><tr><td class="align_left">ρ</td><td class="align_center">24.94</td><td class="align_center">kg/m3</td></tr><tr><td class="align_left">υ12</td><td class="align_center">0.999856</td><td class="align_center">—</td></tr><tr><td class="align_left">υ23</td><td class="align_center">0</td><td class="align_center">—</td></tr><tr><td class="align_left">υ31</td><td class="align_center">0</td><td class="align_center">—</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Equivalent material properties of the honeycomb core.</div>

International Journal of Aerospace Engineering

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Table 2

Table 2: Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method 