<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_61.html"><img src="thumbnails/s61.jpg" width="180" height="67" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide 1: Optimization by GENOPT of an axially compressed cylindrical shell with a composite truss-core sandwich wall"></a></td> <td width="208"><a href="pages/page_62.html"><img src="thumbnails/s62.jpg" width="139" height="180" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide 2: Configuration and decision variables for typical composite truss-core sandwich wall"></a></td> <td width="208"><a href="pages/page_63.html"><img src="thumbnails/s63.jpg" width="180" height="64" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide 3: Part of a model of the truss-core sandwich wall of the cylindrical shell used for the analysis of general buckling"></a></td> <td width="208"><a href="pages/page_64.html"><img src="thumbnails/s64.jpg" width="166" height="180" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide4: General buckling of an optimized axially compressed truss-core sandwich cylindrical shell"></a></td> <td width="208"><a href="pages/page_65.html"><img src="thumbnails/s65.jpg" width="180" height="110" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide 5: Single module of the local buckling model of the axially compressed truss-core sandwich 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">EXAMPLE 7, Slide 1: Optimization by GENOPT of an axially compressed cylindrical shell with a composite truss-core sandwich wall</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 7, Slide 2: Configuration and decision variables for typical composite truss-core sandwich wall</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 7, Slide 3: Part of a model of the truss-core sandwich wall of the cylindrical shell used for the analysis of general buckling</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 7, Slide4: General buckling of an optimized axially compressed truss-core sandwich 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 7, Slide 5: Single module of the local buckling model of the axially compressed truss-core sandwich 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_66.html"><img src="thumbnails/s66.jpg" width="180" height="47" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide 6: Local buckling of part of an axially compressed cylindrical shell with a truss-core sandwich wall construction"></a></td> <td width="208"><a href="pages/page_67.html"><img src="thumbnails/s67.jpg" width="179" height="137" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide 7: Behaviors, design margins, and weight/area of a GENOPT-optimized, axially compressed, composite, truss-core sandwich cylinder"></a></td> <td width="208"><a href="pages/page_68.html"><img src="thumbnails/s68.jpg" width="180" height="140" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide 8: Part of a STAGS model of an axially compressed optimized cylindrical shell with a truss-core sandwich wall"></a></td> <td width="208"><a href="pages/page_69.html"><img src="thumbnails/s69.jpg" width="141" height="180" border="0" hspace="14" vspace="0" alt="EXAMPLE 7, Slide 9: Local buckling of part of the axially compressed optimized cylinder from the STAGS model of the type displayed one slide ago "></a></td> <td width="208"><a href="pages/page_70.html"><img src="thumbnails/s70.jpg" width="180" height="48" border="0" hspace="14" vspace="0" alt="EXAMPLE 8, Slide 1: Optimization of double-walled spherical and cylindrical "balloons""></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 7, Slide 6: Local buckling of part of an axially compressed cylindrical shell with a truss-core sandwich wall construction</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 7, Slide 7: Behaviors, design margins, and weight/area of a GENOPT-optimized, axially compressed, composite, truss-core sandwich cylinder</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 7, Slide 8: Part of a STAGS model of an axially compressed optimized cylindrical shell with a truss-core sandwich wall</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 7, Slide 9: Local buckling of part of the axially compressed optimized cylinder from the STAGS model of the type displayed one slide ago </small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 8, Slide 1: Optimization of double-walled spherical and cylindrical "balloons"</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_71.html"><img src="thumbnails/s71.jpg" width="169" height="180" border="0" hspace="14" vspace="0" alt="EXAMPLE 8, Slide 2: Double-walled optimized spherical balloon with 15 modules with radial webs over 90 degrees of meridian"></a></td> <td width="208"><a href="pages/page_72.html"><img src="thumbnails/s72.jpg" width="170" height="180" border="0" hspace="14" vspace="0" alt="EXAMPLE 8, Slide 3: Double-walled optimized spherical balloon with 15 modules of truss-like (slanted) webs over 90 degrees of meridian"></a></td> <td width="208"><a href="pages/page_73.html"><img src="thumbnails/s73.jpg" width="167" height="180" border="0" hspace="14" vspace="0" alt="EXAMPLE 8, Slide 4: Local buckling of optimized double-walled spherical balloon with 8 truss-like modules over 90 degrees of meridian"></a></td> <td width="208"><a href="pages/page_74.html"><img src="thumbnails/s74.jpg" width="160" height="180" border="0" hspace="14" vspace="0" alt="EXAMPLE 8, Slide 5: Optimized weights of spherical balloons made of polyethelene terephthalate versus the number of modules over 90 meridional degrees"></a></td> <td width="208"><a href="pages/page_75.html"><img src="thumbnails/s75.jpg" width="166" height="180" border="0" hspace="14" vspace="0" alt="EXAMPLE 8, Slide 6: Local buckling of optimized spherical balloon made of polyethylene terephthalate; 35 truss-like modules over 90 meridional degrees"></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 8, Slide 2: Double-walled optimized spherical balloon with 15 modules with radial webs over 90 degrees of meridian</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 8, Slide 3: Double-walled optimized spherical balloon with 15 modules of truss-like (slanted) webs over 90 degrees of meridian</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 8, Slide 4: Local buckling of optimized double-walled spherical balloon with 8 truss-like modules over 90 degrees of meridian</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 8, Slide 5: Optimized weights of spherical balloons made of polyethelene terephthalate versus the number of modules over 90 meridional degrees</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">EXAMPLE 8, Slide 6: Local buckling of optimized spherical balloon made of polyethylene terephthalate; 35 truss-like modules over 90 meridional degrees</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

genopt pictures

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

Generated by Galerie
Wednesday, September 3, 2014