<table cellspacing="0" cellpadding="0" border="0"> <tr><td height="14"></td></tr> <tr align="center" valign="middle"> <td width="188"><a href="pages/page_31.html"><img src="thumbnails/s31.jpg" width="160" height="110" border="0" hspace="14" vspace="0" alt="STAGS model for local buckling of the axially compressed cylindrical shell with a composite truss-core sandwich wall"></a></td> <td width="188"><a href="pages/page_32.html"><img src="thumbnails/s32.jpg" width="160" height="68" border="0" hspace="14" vspace="0" alt="Part of the STAGS model of an axially compressed cylindrical shell with a composite truss-core sandwich wall"></a></td> <td width="188"><a href="pages/page_33.html"><img src="thumbnails/s33.jpg" width="160" height="128" border="0" hspace="14" vspace="0" alt="General buckling of the axially compressed cylindrical shell with a truss-core sandwich wall"></a></td> <td width="188"><a href="pages/page_34.html"><img src="thumbnails/s34.jpg" width="110" height="160" border="0" hspace="14" vspace="0" alt="Static and dynamic buckling process of a graphite-epoxy composite cylindrical shell under uniform end shortening"></a></td> <td width="188"><a href="pages/page_35.html"><img src="thumbnails/s35.jpg" width="160" height="151" border="0" hspace="14" vspace="0" alt="Kinetic energy versus time during the transient phase of the STAGS analysis of the axially compressed composite cylindrical shell shown in the previou"></a></td> </tr> <tr><td height="5"></td></tr> <tr align="center" valign="top"> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">STAGS model for local buckling of the axially compressed cylindrical shell with a composite truss-core sandwich wall</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Part of the STAGS model of an axially compressed cylindrical shell with a composite truss-core sandwich wall</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">General buckling of the axially compressed cylindrical shell with a truss-core sandwich wall</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Static and dynamic buckling process of a graphite-epoxy composite cylindrical shell under uniform end shortening</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Kinetic energy versus time during the transient phase of the STAGS analysis of the axially compressed composite cylindrical shell shown in the previou</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

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Monday, February 6, 2012