<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="180" height="137" border="0" hspace="14" vspace="0" alt="Buckling of stiffened curved panel with sub-stiffeners under combined loads. This is an intermediate-sized sub-domain model of a 360-deg. cyl. shell "></a></td> <td width="208"><a href="pages/page_92.html"><img src="thumbnails/s92.jpg" width="180" height="172" border="0" hspace="14" vspace="0" alt="Buckling of the optimized complete cylindrical shell with smeared sub-stiffeners"></a></td> <td width="208"><a href="pages/page_93.html"><img src="thumbnails/s93.jpg" width="114" height="180" border="0" hspace="14" vspace="0" alt="Optimized ring-Stiffened cylindrical shell under external hydrostatic pressure: General and local skin buckling from PANDA2, BOSOR4 and STAGS"></a></td> <td width="208"><a href="pages/page_94.html"><img src="thumbnails/s94.jpg" width="180" height="171" border="0" hspace="14" vspace="0" alt="General buckling mode from STAGS of an optimized T-ring-stiffened cylindrical shell under external pressure"></a></td> <td width="208"><a href="pages/page_95.html"><img src="thumbnails/s95.jpg" width="180" height="135" border="0" hspace="14" vspace="0" alt="Typical repeating section of a hat-stiffened axially compressed panel"></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 stiffened curved panel with sub-stiffeners under combined loads. This is an intermediate-sized sub-domain model of a 360-deg. cyl. shell </small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of the optimized complete cylindrical shell with smeared sub-stiffeners</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Optimized ring-Stiffened cylindrical shell under external hydrostatic pressure: General and local skin buckling from PANDA2, BOSOR4 and STAGS</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">General buckling mode from STAGS of an optimized T-ring-stiffened cylindrical shell under external pressure</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Typical repeating section of a hat-stiffened axially compressed panel</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="176" height="180" border="0" hspace="14" vspace="0" alt="Global model of a curved axially compressed hat-stiffened panel with local and "global" buckling modes"></a></td> <td width="208"><a href="pages/page_97.html"><img src="thumbnails/s97.jpg" width="180" height="113" border="0" hspace="14" vspace="0" alt="Schematics of local and global buckling of and axially compressed stiffened panel"></a></td> <td width="208"><a href="pages/page_98.html"><img src="thumbnails/s98.jpg" width="180" height="153" border="0" hspace="14" vspace="0" alt="Composite stiffened panel under combined in-plane shear and axial compression"></a></td> <td width="208"><a href="pages/page_99.html"><img src="thumbnails/s99.jpg" width="180" height="163" border="0" hspace="14" vspace="0" alt="Stiffened panel with sub-stiffened skin"></a></td> <td width="208"><a href="pages/page_100.html"><img src="thumbnails/s100.jpg" width="179" height="129" border="0" hspace="14" vspace="0" alt="Axially compressed orthogrid stiffened and sub-stiffened 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">Global model of a curved axially compressed hat-stiffened panel with local and "global" buckling modes</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Schematics of local and global buckling of and axially compressed stiffened panel</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Composite stiffened panel under combined in-plane shear and axial compression</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Stiffened panel with sub-stiffened skin</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Axially compressed orthogrid stiffened and sub-stiffened 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="180" height="130" border="0" hspace="14" vspace="0" alt="Imperfection sensitivity of optimized axially compressed traditionally stiffened and hierarchically stiffened cylindrical shells "></a></td> <td width="208"><a href="pages/page_102.html"><img src="thumbnails/s102.jpg" width="180" height="101" border="0" hspace="14" vspace="0" alt="Analysis of a longitudinally stiffened panel with use of the strip method"></a></td> <td width="208"><a href="pages/page_103.html"><img src="thumbnails/s103.jpg" width="180" height="103" border="0" hspace="14" vspace="0" alt="Local and later general buckling of the longitudinally stiffened, axially compressed panel"></a></td> <td width="208"><a href="pages/page_104.html"><img src="thumbnails/s104.jpg" width="180" height="77" border="0" hspace="14" vspace="0" alt="Introduction of an interface layer in order to predict the onset of delamination"></a></td> <td width="208"><a href="pages/page_105.html"><img src="thumbnails/s105.jpg" width="180" height="56" border="0" hspace="14" vspace="0" alt="Buckling of stiffened panel: local (left), stiffener (middle), general (right)"></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">Imperfection sensitivity of optimized axially compressed traditionally stiffened and hierarchically stiffened cylindrical shells </small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Analysis of a longitudinally stiffened panel with use of the strip method</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Local and later general buckling of the longitudinally stiffened, axially compressed panel</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Introduction of an interface layer in order to predict the onset of delamination</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of stiffened panel: local (left), stiffener (middle), general (right)</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

stiffened cylindrical shells

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Sunday, December 27, 2020