<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>

Crippling of the core of a sandwich panel under normal compression and 3 and 4 point bending	Crashworthiness of various cellular configuration under out-of-plane crushing impact	Geometries of sandwich cores to be tested under vertical shock loading	Quasi-static test of square honeycomb sample	Crushing of auxetic sandwich core under blast loading
Sandwich wall with pyramidal truss core [28]	Various composite lattice (truss) core sandwich configurations [28]	Truss-core sandwich panel loaded in compression (pressure) normal to the upper surface	Formation of lattice grids for sandwich core [32]	Making a lattice core sandwich cylindrical shell
Buckling of a single cell of a square honeycomb under axial compression (compression in the plane of the walls of a cell)	Buckling of hexagonal honeycomb under axial compression	Test rig configuration for dynamic crushing of sandwich specimens with various core geometries	Results from test and finite element models for sandwich specimens with square honeycomb core	Aluminum sandwich panel: Effect of local low-velocity impact normal to the upper face sheet

sandwich shells

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Monday, December 28, 2020