<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_21.html"><img src="thumbnails/s21.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="STAGS model of a T-ring and T-stringer stiffened cylindrical shell under combined loading"></a></td> <td width="188"><a href="pages/page_22.html"><img src="thumbnails/s22.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="General buckling of a perfect ring and stringer-stiffened cylindrical shell under combined axial compression and external pressure"></a></td> <td width="188"><a href="pages/page_23.html"><img src="thumbnails/s23.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Inter-ring buckling of an imperfect ring and stringer-stiffened cylindrical shell under combined axial compression and external pressure"></a></td> <td width="188"><a href="pages/page_24.html"><img src="thumbnails/s24.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Collapse of an imperfect, T-stiffened, optimized cylindrical shell under combined axial compression, external pressure, and torque"></a></td> <td width="188"><a href="pages/page_25.html"><img src="thumbnails/s25.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="STAGS model of the imperfect, axially compressed, ring and stringer stiffened cylindrical shell optimized by PANDA2"></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 of a T-ring and T-stringer stiffened cylindrical shell under combined loading</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 a perfect ring and stringer-stiffened cylindrical shell under combined axial compression and external pressure</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Inter-ring buckling of an imperfect ring and stringer-stiffened cylindrical shell under combined axial compression and external pressure</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Collapse of an imperfect, T-stiffened, optimized cylindrical shell under combined axial compression, external pressure, and torque</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">STAGS model of the imperfect, axially compressed, ring and stringer stiffened cylindrical shell optimized by PANDA2</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_26.html"><img src="thumbnails/s26.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Non-axisymmetric buckling mode from STAGS for an ellipsoidal shell optimized by GENOPT"></a></td> <td width="188"><a href="pages/page_27.html"><img src="thumbnails/s27.jpg" width="160" height="138" border="0" hspace="14" vspace="0" alt="STAGS model of axially compressed cylindrical panel with half of a T-stiffened weld land (top) and including one ring bay"></a></td> <td width="188"><a href="pages/page_28.html"><img src="thumbnails/s28.jpg" width="160" height="136" border="0" hspace="14" vspace="0" alt="General buckling mode from a 120-degree STAGS model of the optimized internally stiffened cylindrical shell with T-stiffened weld lands"></a></td> <td width="188"><a href="pages/page_29.html"><img src="thumbnails/s29.jpg" width="160" height="108" border="0" hspace="14" vspace="0" alt="Maximum effective stress predicted by a 60-degree STAGS model of the optimized internally stiffened cylindrical shell with T-stiffened weld lands"></a></td> <td width="188"><a href="pages/page_30.html"><img src="thumbnails/s30.jpg" width="160" height="124" border="0" hspace="14" vspace="0" alt="Part of a STAGS model of an axially compressed cylindrical shell with a truss-core sandwich wall"></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">Non-axisymmetric buckling mode from STAGS for an ellipsoidal shell optimized by GENOPT</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">STAGS model of axially compressed cylindrical panel with half of a T-stiffened weld land (top) and including one ring bay</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">General buckling mode from a 120-degree STAGS model of the optimized internally stiffened cylindrical shell with T-stiffened weld lands</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Maximum effective stress predicted by a 60-degree STAGS model of the optimized internally stiffened cylindrical shell with T-stiffened weld lands</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Part of a STAGS model of an axially compressed cylindrical shell with a truss-core sandwich wall</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

stags pictures

Click on a photo to see more information and (in most cases) to see a larger image.

Generated by Galerie
Monday, February 6, 2012