<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_11.html"><img src="thumbnails/s11.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Local skin buckling in a STAGS sub-domain model of a blade-stiffened cylindrical shell under combined Nx and Nxy"></a></td> <td width="188"><a href="pages/page_12.html"><img src="thumbnails/s12.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="STAGS sub-domain model of Inter-ring buckling of a Z-ring and Z-stringer stiffened cylindrical shell under combined Nx and Nxy"></a></td> <td width="188"><a href="pages/page_13.html"><img src="thumbnails/s13.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="STAGS model of inter-ring buckling of a T-ring and T-stringer stiffened cylindrical shell under combined loading Nx and Nxy"></a></td> <td width="188"><a href="pages/page_14.html"><img src="thumbnails/s14.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="STAGS model of the T-ring and T-stringer stiffened cylindrical shell at the load combination, Nx and Nxy, that causes ultimate collapse of the shell"></a></td> <td width="188"><a href="pages/page_15.html"><img src="thumbnails/s15.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="STAGS model of collapse of the blade-stiffened cylindrical shell under combined Nx and Nxy"></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">Local skin buckling in a STAGS sub-domain model of a blade-stiffened cylindrical shell under combined Nx and Nxy</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">STAGS sub-domain model of Inter-ring buckling of a Z-ring and Z-stringer stiffened cylindrical shell under combined Nx and Nxy</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 inter-ring buckling of a T-ring and T-stringer stiffened cylindrical shell under combined loading Nx and Nxy</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 T-ring and T-stringer stiffened cylindrical shell at the load combination, Nx and Nxy, that causes ultimate collapse of the shell</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 collapse of the blade-stiffened cylindrical shell under combined Nx and Nxy</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_16.html"><img src="thumbnails/s16.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Extreme fiber axial strain, eps(xx), versus load factor, PA"></a></td> <td width="188"><a href="pages/page_17.html"><img src="thumbnails/s17.jpg" width="160" height="81" border="0" hspace="14" vspace="0" alt="Title and abstract from a 2005 PANDA2 paper about panels with major stiffeners and sub-stiffeners in the bays between adjacent major stiffeners"></a></td> <td width="188"><a href="pages/page_18.html"><img src="thumbnails/s18.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Starting and optimum designs of perfect and imperfect cylindrical shells with T-shaped major stiffeners and blade-shaped sub-stiffeners"></a></td> <td width="188"><a href="pages/page_19.html"><img src="thumbnails/s19.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="STAGS sub-domain model of a PANDA2-optimized perfect cylindrical shell under combined loads, Nx, Ny, Nxy, p"></a></td> <td width="188"><a href="pages/page_20.html"><img src="thumbnails/s20.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Objective vs. design iterations during PANDA2 optimization of the stiffened and sub-stiffened cylindrical shell under combined loads, Nx, Ny, Nxy, p "></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">Extreme fiber axial strain, eps(xx), versus load factor, PA</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Title and abstract from a 2005 PANDA2 paper about panels with major stiffeners and sub-stiffeners in the bays between adjacent major stiffeners</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Starting and optimum designs of perfect and imperfect cylindrical shells with T-shaped major stiffeners and blade-shaped sub-stiffeners</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">STAGS sub-domain model of a PANDA2-optimized perfect cylindrical shell under combined loads, Nx, Ny, Nxy, p</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Objective vs. design iterations during PANDA2 optimization of the stiffened and sub-stiffened cylindrical shell under combined loads, Nx, Ny, Nxy, p </small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

panda2 2002-07

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Monday, February 6, 2012