<table cellspacing="0" cellpadding="0" border="0"> <tr><td height="14"></td></tr> <tr align="center" valign="middle"> <td width="208"><a href="pages/page_91.html"><img src="thumbnails/s91.jpg" width="117" height="180" border="0" hspace="14" vspace="0" alt="Crippling of the core of a sandwich panel under normal compression and 3 and 4 point bending"></a></td> <td width="208"><a href="pages/page_92.html"><img src="thumbnails/s92.jpg" width="180" height="96" border="0" hspace="14" vspace="0" alt="Crashworthiness of various cellular configuration under out-of-plane crushing impact"></a></td> <td width="208"><a href="pages/page_93.html"><img src="thumbnails/s93.jpg" width="180" height="135" border="0" hspace="14" vspace="0" alt="Geometries of sandwich cores to be tested under vertical shock loading"></a></td> <td width="208"><a href="pages/page_94.html"><img src="thumbnails/s94.jpg" width="180" height="132" border="0" hspace="14" vspace="0" alt="Quasi-static test of square honeycomb sample"></a></td> <td width="208"><a href="pages/page_95.html"><img src="thumbnails/s95.jpg" width="179" height="94" border="0" hspace="14" vspace="0" alt="Crushing of auxetic sandwich core under blast loading"></a></td> </tr> <tr><td height="5"></td></tr> <tr align="center" valign="top"> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Crippling of the core of a sandwich panel under normal compression and 3 and 4 point bending</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Crashworthiness of various cellular configuration under out-of-plane crushing impact</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Geometries of sandwich cores to be tested under vertical shock loading</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Quasi-static test of square honeycomb sample</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Crushing of auxetic sandwich core under blast loading</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> <tr><td height="14"></td></tr> <tr align="center" valign="middle"> <td width="208"><a href="pages/page_96.html"><img src="thumbnails/s96.jpg" width="180" height="92" border="0" hspace="14" vspace="0" alt="Sandwich wall with pyramidal truss core [28]"></a></td> <td width="208"><a href="pages/page_97.html"><img src="thumbnails/s97.jpg" width="180" height="102" border="0" hspace="14" vspace="0" alt="Various composite lattice (truss) core sandwich configurations [28]"></a></td> <td width="208"><a href="pages/page_98.html"><img src="thumbnails/s98.jpg" width="180" height="78" border="0" hspace="14" vspace="0" alt="Truss-core sandwich panel loaded in compression (pressure) normal to the upper surface"></a></td> <td width="208"><a href="pages/page_99.html"><img src="thumbnails/s99.jpg" width="180" height="74" border="0" hspace="14" vspace="0" alt="Formation of lattice grids for sandwich core [32]"></a></td> <td width="208"><a href="pages/page_100.html"><img src="thumbnails/s100.jpg" width="180" height="65" border="0" hspace="14" vspace="0" alt="Making a lattice core sandwich cylindrical shell"></a></td> </tr> <tr><td height="5"></td></tr> <tr align="center" valign="top"> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Sandwich wall with pyramidal truss core [28]</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Various composite lattice (truss) core sandwich configurations [28]</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Truss-core sandwich panel loaded in compression (pressure) normal to the upper surface</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Formation of lattice grids for sandwich core [32]</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Making a lattice core sandwich cylindrical shell</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> <tr><td height="14"></td></tr> <tr align="center" valign="middle"> <td width="208"><a href="pages/page_101.html"><img src="thumbnails/s101.jpg" width="136" height="180" border="0" hspace="14" vspace="0" alt="Buckling of a single cell of a square honeycomb under axial compression (compression in the plane of the walls of a cell)"></a></td> <td width="208"><a href="pages/page_102.html"><img src="thumbnails/s102.jpg" width="180" height="169" border="0" hspace="14" vspace="0" alt="Buckling of hexagonal honeycomb under axial compression"></a></td> <td width="208"><a href="pages/page_103.html"><img src="thumbnails/s103.jpg" width="180" height="158" border="0" hspace="14" vspace="0" alt="Test rig configuration for dynamic crushing of sandwich specimens with various core geometries"></a></td> <td width="208"><a href="pages/page_104.html"><img src="thumbnails/s104.jpg" width="180" height="137" border="0" hspace="14" vspace="0" alt="Results from test and finite element models for sandwich specimens with square honeycomb core"></a></td> <td width="208"><a href="pages/page_105.html"><img src="thumbnails/s105.jpg" width="180" height="110" border="0" hspace="14" vspace="0" alt="Aluminum sandwich panel: Effect of local low-velocity impact normal to the upper face sheet"></a></td> </tr> <tr><td height="5"></td></tr> <tr align="center" valign="top"> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of a single cell of a square honeycomb under axial compression (compression in the plane of the walls of a cell)</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of hexagonal honeycomb under axial compression</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Test rig configuration for dynamic crushing of sandwich specimens with various core geometries</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Results from test and finite element models for sandwich specimens with square honeycomb core</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Aluminum sandwich panel: Effect of local low-velocity impact normal to the upper face sheet</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

sandwich shells

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Monday, December 28, 2020