<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="Extenally pressurized ellipsoidal shell with thickness that varies along the meridian"></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="Internally pressurized ellispoidal tank and the maximum stress predicted by BOSOR4/BIGBOSOR4 from linear and nonlinear models"></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="Comparison of convergence with respect to nodal point density along the meridian of a shell of revolution"></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="Part of a shell of revolution, showing the nodal degrees of freedom for a single finite difference energy "element""></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="Some prismatic structures that can be analyzed by BOSOR4/BIGBOSOR4"></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">Extenally pressurized ellipsoidal shell with thickness that varies along the meridian</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Internally pressurized ellispoidal tank and the maximum stress predicted by BOSOR4/BIGBOSOR4 from linear and nonlinear models</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Comparison of convergence with respect to nodal point density along the meridian of a shell of revolution</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 shell of revolution, showing the nodal degrees of freedom for a single finite difference energy "element"</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Some prismatic structures that can be analyzed by BOSOR4/BIGBOSOR4</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-circular cylindrical shell with circumferentially varying external pressure modeled as part of a huge torus"></a></td> <td width="188"><a href="pages/page_27.html"><img src="thumbnails/s27.jpg" width="160" height="151" border="0" hspace="14" vspace="0" alt="Huge torus model of a cylindrical shell of length L (Drawing by Robert P. Thornburgh)"></a></td> <td width="188"><a href="pages/page_28.html"><img src="thumbnails/s28.jpg" width="160" height="111" border="0" hspace="14" vspace="0" alt="In 2010 the capability to analyze true prismatic shells was implemented in BIGBOSOR4"></a></td> <td width="188"><a href="pages/page_29.html"><img src="thumbnails/s29.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Buckling of axially compressed, semi-sandwich corrugated panels by BIGBOSOR4"></a></td> <td width="188"><a href="pages/page_30.html"><img src="thumbnails/s30.jpg" width="143" height="160" border="0" hspace="14" vspace="0" alt="Axially compressed cylindrical shell with six weld lands with T-shaped stringers, analyzed as a true prismatic structure by BIGBOSOR4"></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-circular cylindrical shell with circumferentially varying external pressure modeled as part of a huge torus</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Huge torus model of a cylindrical shell of length L (Drawing by Robert P. Thornburgh)</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">In 2010 the capability to analyze true prismatic shells was implemented in BIGBOSOR4</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of axially compressed, semi-sandwich corrugated panels by BIGBOSOR4</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Axially compressed cylindrical shell with six weld lands with T-shaped stringers, analyzed as a true prismatic structure by BIGBOSOR4</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

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Monday, February 6, 2012