<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_1.html"><img src="thumbnails/s1.jpg" width="134" height="160" border="0" hspace="14" vspace="0" alt="Information about STAGS (slide 1 of 2)"></a></td> <td width="188"><a href="pages/page_2.html"><img src="thumbnails/s2.jpg" width="143" height="160" border="0" hspace="14" vspace="0" alt="Information about STAGS (slide 2 of 2)"></a></td> <td width="188"><a href="pages/page_3.html"><img src="thumbnails/s3.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Post-buckling of a stiffened shear panel as analyzed by the STAGS computer program"></a></td> <td width="188"><a href="pages/page_4.html"><img src="thumbnails/s4.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Postbuckling deformation from STAGS of an externally blade-stiffened cylindrical metallic panel under combined axial compression and in-plane shear"></a></td> <td width="188"><a href="pages/page_5.html"><img src="thumbnails/s5.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Plan view of postbuckling deformation of a T-stiffened panel under combined axial compression, in-plane shear and normal pressure"></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">Information about STAGS (slide 1 of 2)</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Information about STAGS (slide 2 of 2)</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Post-buckling of a stiffened shear panel as analyzed by the STAGS computer program</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Postbuckling deformation from STAGS of an externally blade-stiffened cylindrical metallic panel under combined axial compression and in-plane shear</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Plan view of postbuckling deformation of a T-stiffened panel under combined axial compression, in-plane shear and normal pressure</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="188"><a href="pages/page_6.html"><img src="thumbnails/s6.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Two views of the local buckling mode of a flat panel under combined axial compression, in-plane shear and normal pressure"></a></td> <td width="188"><a href="pages/page_7.html"><img src="thumbnails/s7.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="STAGS prediction of contours of normal displacement in the far-postbuckling regime"></a></td> <td width="188"><a href="pages/page_8.html"><img src="thumbnails/s8.jpg" width="121" height="160" border="0" hspace="14" vspace="0" alt="Nonlinear static post-buckling STAGS analysis of an axially compressed, axially stiffened panel previously optimized by PANDA2"></a></td> <td width="188"><a href="pages/page_9.html"><img src="thumbnails/s9.jpg" width="120" height="160" border="0" hspace="14" vspace="0" alt="A three-phase nonlinear STAGS analysis of a stiffened panel previously optimized by PANDA2"></a></td> <td width="188"><a href="pages/page_10.html"><img src="thumbnails/s10.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Time sequence of local post-buckling deformations in an axially compressed blade-stiffened flat panel"></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">Two views of the local buckling mode of a flat panel under combined axial compression, in-plane shear and normal pressure</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">STAGS prediction of contours of normal displacement in the far-postbuckling regime</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Nonlinear static post-buckling STAGS analysis of an axially compressed, axially stiffened panel previously optimized by PANDA2</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">A three-phase nonlinear STAGS analysis of a stiffened panel previously optimized by PANDA2</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Time sequence of local post-buckling deformations in an axially compressed blade-stiffened flat panel</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

stags pictures

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Monday, February 6, 2012