Numerical and Experimental Investigation of Wrinkling Pattern for Aerospace Laminated Membrane Structures

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Type</td><td class="align_center">SB102</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Size of table board (mm)</td><td class="align_center">300 × 600 × 13</td></tr><tr><td class="align_left">Flatness</td><td class="align_center">0.08 mm/m<sup>2</sup></td></tr><tr><td class="align_left">Pitch row</td><td class="align_center">25 mm × 25 mm</td></tr><tr><td class="align_left">Aperture</td><td class="align_center">M6</td></tr><tr><td class="align_left">Material</td><td class="align_center">High-quality aluminum alloy</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Technical characteristics of SB102 optical plate.

International Journal of Aerospace Engineering

tab3

Table 3

Table 3: Numerical and Experimental Investigation of Wrinkling Pattern for Aerospace Laminated Membrane Structures 