<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_151.html"><img src="thumbnails/s151.jpg" width="180" height="168" border="0" hspace="14" vspace="0" alt="Example 11, Slide 10: Starting design and optimized designs of a corrugated panel with sub-segments"></a></td> <td width="208"><a href="pages/page_152.html"><img src="thumbnails/s152.jpg" width="180" height="131" border="0" hspace="14" vspace="0" alt="Example 11, Slide 11: STAGS finite element model of the same panel previously optimized by GENOPT/BIGBOSOR4"></a></td> <td width="208"><a href="pages/page_153.html"><img src="thumbnails/s153.jpg" width="180" height="112" border="0" hspace="14" vspace="0" alt="Example 11, Slide 12: Lowest buckling mode from the STAGS finite element model shown in the previous slide"></a></td> <td width="208"><a href="pages/page_154.html"><img src="thumbnails/s154.jpg" width="148" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 13: Sensitivity of the optimized design to one of the decision variables, YPLATE(8)"></a></td> <td width="208"><a href="pages/page_155.html"><img src="thumbnails/s155.jpg" width="147" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 14: Sensitivity of the optimized design to another of the decision variables, YPLATE(9)"></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">Example 11, Slide 10: Starting design and optimized designs of a corrugated panel with sub-segments</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 11: STAGS finite element model of the same panel previously optimized 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">Example 11, Slide 12: Lowest buckling mode from the STAGS finite element model shown in the previous slide</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 13: Sensitivity of the optimized design to one of the decision variables, YPLATE(8)</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 14: Sensitivity of the optimized design to another of the decision variables, YPLATE(9)</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_156.html"><img src="thumbnails/s156.jpg" width="173" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 15: Strategy for "smoothing" a cross-section profile with corners"></a></td> <td width="208"><a href="pages/page_157.html"><img src="thumbnails/s157.jpg" width="160" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 16: Zoomed view of the strategy for "smoothing" a cross-section profile with corners"></a></td> <td width="208"><a href="pages/page_158.html"><img src="thumbnails/s158.jpg" width="177" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 17: Smoothing strategy, optimized smoothed cross section, extended panel"></a></td> <td width="208"><a href="pages/page_159.html"><img src="thumbnails/s159.jpg" width="180" height="149" border="0" hspace="14" vspace="0" alt="Example 11, Slide 18: Optimization of a panel with shallower cylindrical segments. This panel can be fabricated by stamping"></a></td> <td width="208"><a href="pages/page_160.html"><img src="thumbnails/s160.jpg" width="178" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 19: The optimized "flat" panel shown 10 slides ago is mapped onto a cylindrical surface"></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">Example 11, Slide 15: Strategy for "smoothing" a cross-section profile with corners</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 16: Zoomed view of the strategy for "smoothing" a cross-section profile with corners</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 17: Smoothing strategy, optimized smoothed cross section, extended panel</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 18: Optimization of a panel with shallower cylindrical segments. This panel can be fabricated by stamping</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 19: The optimized "flat" panel shown 10 slides ago is mapped onto a cylindrical surface</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_161.html"><img src="thumbnails/s161.jpg" width="179" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 20: General buckling mode of the mapped corrugated cylindrical shell"></a></td> <td width="208"><a href="pages/page_162.html"><img src="thumbnails/s162.jpg" width="180" height="179" border="0" hspace="14" vspace="0" alt="Example 11, Slide 21:"></a></td> <td width="208"><a href="pages/page_163.html"><img src="thumbnails/s163.jpg" width="172" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 22:"></a></td> <td width="208"><a href="pages/page_164.html"><img src="thumbnails/s164.jpg" width="143" height="180" border="0" hspace="14" vspace="0" alt="Example 11, Slide 23: Buckling of optimized axially compressed aluminum cylindrical shell with external T-shaped stringers"></a></td> <td width="208"><a href="pages/page_165.html"><img src="thumbnails/s165.jpg" width="163" height="179" border="0" hspace="14" vspace="0" alt="Example 11, Slide 24: Buckling of optimized axially compressed aluminum cylindrical shell with a truss-core sandwich wall"></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">Example 11, Slide 20: General buckling mode of the mapped corrugated cylindrical shell</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 21:</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 22:</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 23: Buckling of optimized axially compressed aluminum cylindrical shell with external T-shaped stringers</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Example 11, Slide 24: Buckling of optimized axially compressed aluminum cylindrical shell with a truss-core sandwich wall</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

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Wednesday, September 3, 2014