Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td class="align_left">Ten stress fiber dir (MPa)</td><td class="align_center">Com stress fiber dir (MPa)</td><td class="align_center">Ten stress transv dir (MPa)</td><td class="align_center">Com stress transv dir (MPa)</td><td class="align_center">Shear strength (MPa)</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td class="align_left">724.64</td><td class="align_center">546.06</td><td class="align_center">320.61</td><td class="align_center">261.31</td><td class="align_center">206.125</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>T300/epoxy composite properties [<a href="/journals/ijae/2022/3768195/#B9" target="_blank">9</a>, <a href="/journals/ijae/2022/3768195/#B10" target="_blank">10</a>].</div>

International Journal of Aerospace Engineering

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Table 3

Table 3: Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration 

Table 3 | Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration 