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="tab8"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Work conditions</td><td class="align_center">Strain cloud map</td><td class="align_center">Maximum strain</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Short side sheared</td><td class="align_center"><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/3768195/figures/3768195.tab-inline.005.svgz" name="3768195.tab-inline.005" type="image/svg+xml"></object></td><td class="align_center"><span style="width: 62.1637ptpx;"><svg height="8.98583pt" id="M15" style="vertical-align:-0.3499308pt" version="1.1" viewbox="-0.0498162 -8.6359 62.1637 8.98583" width="62.1637pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M384 0V27C293 34 287 42 287 114V635C232 613 172 594 109 583V559L157 557C201 555 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<div>Strain cloud under typical static load.</div>

International Journal of Aerospace Engineering

tab8

Table 8

Table 8: 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 8 | 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 