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| A concept for a deployable wing |
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| Deep drawing (forming) of a woven fabric composite |
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| The amount of edge wrinkling diminishes with increasing second-gradient parameter, alpha |
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| Wrinkling of a composite sheet draped over a cylindrical solid |
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| Wrinkling under lengthwise compression of a woven strip with different bending stiffnesses |
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| Morphing lattice boom at two stages during deployment |
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| Fully deployed morphing lattice boom |
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| Convergence of the normal displacement under the downward concentrated load P with increasing number of nodal points |
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| Single-walled carbon nanotubes and the dependence of vibration frequency on the nonlocal parameter mu |
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| (a),(b) Local buckling; (c),(d) General Buckling of a metamaterial |
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| Deformation of a vertically compressed 50x50x6.36 mm slab with oval-shaped perforations |
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| Complex cellular structures to be crushed |
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| Example of crushing of a cellular structure: Comparison of test and theory |
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| Crushing force-displacement curves from test and theory |
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| Very large displacements of a beam |
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