<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_16.html"><img src="thumbnails/s16.jpg" width="180" height="106" border="0" hspace="14" vspace="0" alt="Flexural-Torsional buckling of axially compressed cruciform column with flanges"></a></td> <td width="208"><a href="pages/page_17.html"><img src="thumbnails/s17.jpg" width="180" height="80" border="0" hspace="14" vspace="0" alt="Buckling of oval cylindrical shell in bending"></a></td> <td width="208"><a href="pages/page_18.html"><img src="thumbnails/s18.jpg" width="167" height="180" border="0" hspace="14" vspace="0" alt="General buckling mode of optimized cylindrical balloon with 40 truss-like modules over 90 degrees of circumference"></a></td> <td width="208"><a href="pages/page_19.html"><img src="thumbnails/s19.jpg" width="180" height="97" border="0" hspace="14" vspace="0" alt="Longitudinally corrugated long cylindrical shell under external pressure"></a></td> <td width="208"><a href="pages/page_20.html"><img src="thumbnails/s20.jpg" width="180" height="97" border="0" hspace="14" vspace="0" alt="Axially compressed corrugated 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">Flexural-Torsional buckling of axially compressed cruciform column with flanges</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of oval cylindrical shell in bending</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 of optimized cylindrical balloon with 40 truss-like modules over 90 degrees of circumference</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Longitudinally corrugated long 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">Axially compressed corrugated 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_21.html"><img src="thumbnails/s21.jpg" width="180" height="61" border="0" hspace="14" vspace="0" alt="Both perfect and imperfect shells are considered in our optimization. (a) Perfect wavy shell. (b) Imperfection shape based on critical buckling mode. "></a></td> <td width="208"><a href="pages/page_22.html"><img src="thumbnails/s22.jpg" width="159" height="179" border="0" hspace="14" vspace="0" alt="General buckling of optimized, axially compressed corrugated panel"></a></td> <td width="208"><a href="pages/page_23.html"><img src="thumbnails/s23.jpg" width="178" height="180" border="0" hspace="14" vspace="0" alt="Buckling of an optimized, complexly corrugated, axially compressed, cylindrical shell analyzed with HUGEBOSOR4"></a></td> <td width="208"><a href="pages/page_24.html"><img src="thumbnails/s24.jpg" width="180" height="76" border="0" hspace="14" vspace="0" alt="A finite element model of a complexly corrugated cylindrical shell under axial compression previously optimzed by GENOPT/BIGBOSOR4"></a></td> <td width="208"><a href="pages/page_25.html"><img src="thumbnails/s25.jpg" width="180" height="78" border="0" hspace="14" vspace="0" alt="Critical buckling mode of the uniformly axially compressed, complexly corrugated panel shown in the previous slide"></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">Both perfect and imperfect shells are considered in our optimization. (a) Perfect wavy shell. (b) Imperfection shape based on critical buckling mode. </small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">General buckling of optimized, axially compressed corrugated panel</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of an optimized, complexly corrugated, axially compressed, cylindrical shell analyzed with HUGEBOSOR4</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">A finite element model of a complexly corrugated cylindrical shell under axial compression previously optimzed by GENOPT/BIGBOSOR4</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Critical buckling mode of the uniformly axially compressed, complexly corrugated panel shown in the previous slide</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_26.html"><img src="thumbnails/s26.jpg" width="168" height="180" border="0" hspace="14" vspace="0" alt="Another HUGEBOSOR4 model of an optimized, complexly corrugated cylindrical shell with smoothing under uniform axial compression"></a></td> <td width="208"><a href="pages/page_27.html"><img src="thumbnails/s27.jpg" width="157" height="180" border="0" hspace="14" vspace="0" alt="STAGS model of the same optimized, complexly corrugated cylindrical shell with smoothing under uniform axial compression"></a></td> <td width="208"><a href="pages/page_28.html"><img src="thumbnails/s28.jpg" width="180" height="171" border="0" hspace="14" vspace="0" alt="BIGBOSOR4 model of a simpler optimized, complexly corrugated cylindrical shell with smoothing under uniform axial compression"></a></td> <td width="208"><a href="pages/page_29.html"><img src="thumbnails/s29.jpg" width="180" height="156" border="0" hspace="14" vspace="0" alt="STAGS model of the same simpler optimized, complexly corrugated cylindrical shell with smoothing under uniform axial compression"></a></td> <td width="208"><a href="pages/page_30.html"><img src="thumbnails/s30.jpg" width="173" height="180" border="0" hspace="14" vspace="0" alt="The WEIGHT of “global” optimum designs versus number of major segments over WIDTH/2=50 inches"></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">Another HUGEBOSOR4 model of an optimized, complexly corrugated cylindrical shell with smoothing under uniform axial compression</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">STAGS model of the same optimized, complexly corrugated cylindrical shell with smoothing under uniform axial compression</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">BIGBOSOR4 model of a simpler optimized, complexly corrugated cylindrical shell with smoothing under uniform axial compression</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">STAGS model of the same simpler optimized, complexly corrugated cylindrical shell with smoothing under uniform axial compression</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">The WEIGHT of “global” optimum designs versus number of major segments over WIDTH/2=50 inches</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

prismatic shells

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

Generated by Galerie
Sunday, December 27, 2020