<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_31.html"><img src="thumbnails/s31.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Modeling a complete cylindrical shell with circumferentially varying line loads, Nx and Nxy, with one panel subjected to three different combinations "></a></td> <td width="188"><a href="pages/page_32.html"><img src="thumbnails/s32.jpg" width="160" height="116" border="0" hspace="14" vspace="0" alt="The local skin-stringer post-buckling theory used in PANDA2 is described in this paper"></a></td> <td width="188"><a href="pages/page_33.html"><img src="thumbnails/s33.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Postbuckling behavior of an axially compressed unstiffened rectangular plate"></a></td> <td width="188"><a href="pages/page_34.html"><img src="thumbnails/s34.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Local buckling and postbuckling behavior of an axially compressed blade-stiffened panel"></a></td> <td width="188"><a href="pages/page_35.html"><img src="thumbnails/s35.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Local buckling and postbuckling behavior of a composite, axially compressed, T-stiffened panel"></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">Modeling a complete cylindrical shell with circumferentially varying line loads, Nx and Nxy, with one panel subjected to three different combinations </small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">The local skin-stringer post-buckling theory used in PANDA2 is described in this paper</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Postbuckling behavior of an axially compressed unstiffened rectangular plate</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Local buckling and postbuckling behavior of an axially compressed blade-stiffened panel</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Local buckling and postbuckling behavior of a composite, axially compressed, T-stiffened 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="188"><a href="pages/page_36.html"><img src="thumbnails/s36.jpg" width="153" height="160" border="0" hspace="14" vspace="0" alt="Objective versus design iterations during and execution of the PANDA2 processor called "SUPEROPT""></a></td> <td width="188"><a href="pages/page_37.html"><img src="thumbnails/s37.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Move limits of decision variables, X1 and X2, during design iterations in a single execution of the PANDA2 processor, PANDAOPT"></a></td> <td width="188"><a href="pages/page_38.html"><img src="thumbnails/s38.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Objective versus design iterations during 8 successive executions of PANDAOPT"></a></td> <td width="188"><a href="pages/page_39.html"><img src="thumbnails/s39.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Blade stiffened cylindrical panel under combined axial compression and in-plane shear, Nx and Nxy"></a></td> <td width="188"><a href="pages/page_40.html"><img src="thumbnails/s40.jpg" width="123" height="160" border="0" hspace="14" vspace="0" alt="Local postbuckling of the blade stiffened panel shown on the previous slide"></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">Objective versus design iterations during and execution of the PANDA2 processor called "SUPEROPT"</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Move limits of decision variables, X1 and X2, during design iterations in a single execution of the PANDA2 processor, PANDAOPT</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Objective versus design iterations during 8 successive executions of PANDAOPT</small></td></tr></table></td> <td width="188"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Blade stiffened cylindrical panel under combined axial compression and in-plane shear, 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">Local postbuckling of the blade stiffened panel shown on the previous slide</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

panda2 1987-95

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Monday, February 6, 2012