<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_106.html"><img src="thumbnails/s106.jpg" width="180" height="92" border="0" hspace="14" vspace="0" alt="Global Buckling of panel with T-shaped stiffeners"></a></td> <td width="208"><a href="pages/page_107.html"><img src="thumbnails/s107.jpg" width="111" height="180" border="0" hspace="14" vspace="0" alt="The concept of "effective width" used in the study of axially compressed, stiffened, post-locally buckled plates and shells"></a></td> <td width="208"><a href="pages/page_108.html"><img src="thumbnails/s108.jpg" width="180" height="100" border="0" hspace="14" vspace="0" alt="Axially compressed axially stiffened plate buckling and collapse"></a></td> <td width="208"><a href="pages/page_109.html"><img src="thumbnails/s109.jpg" width="179" height="107" border="0" hspace="14" vspace="0" alt="Comparison between test and theory for axially compressed CFRP post-buckled axially stiffened cylindrical panel"></a></td> <td width="208"><a href="pages/page_110.html"><img src="thumbnails/s110.jpg" width="180" height="150" border="0" hspace="14" vspace="0" alt="Numerical prediction by ABAQUS for an axially compressed CFRP post-buckled axially stiffened 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">Global Buckling of panel with T-shaped stiffeners</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">The concept of "effective width" used in the study of axially compressed, stiffened, post-locally buckled plates and shells</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Axially compressed axially stiffened plate buckling and collapse</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Comparison between test and theory for axially compressed CFRP post-buckled axially stiffened cylindrical panel</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Numerical prediction by ABAQUS for an axially compressed CFRP post-buckled axially stiffened 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_111.html"><img src="thumbnails/s111.jpg" width="180" height="160" border="0" hspace="14" vspace="0" alt="Numerical prediction by ABAQUS for a torqued CFRP post-buckled axially stiffened cylindrical shell"></a></td> <td width="208"><a href="pages/page_112.html"><img src="thumbnails/s112.jpg" width="173" height="180" border="0" hspace="14" vspace="0" alt="Nonlinear behavior of CFRP axially stiffened panel under combined axial compression and torque"></a></td> <td width="208"><a href="pages/page_113.html"><img src="thumbnails/s113.jpg" width="180" height="75" border="0" hspace="14" vspace="0" alt="Composite panel: shear buckling (left), pressure buckling (center) and composite strain (right)"></a></td> <td width="208"><a href="pages/page_114.html"><img src="thumbnails/s114.jpg" width="180" height="54" border="0" hspace="14" vspace="0" alt="Buckling modes in in axially compressed stiffened panel"></a></td> <td width="208"><a href="pages/page_115.html"><img src="thumbnails/s115.jpg" width="180" height="79" border="0" hspace="14" vspace="0" alt="Buckling of a typical wing panel under axial compression"></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">Numerical prediction by ABAQUS for a torqued CFRP post-buckled axially stiffened cylindrical shell</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Nonlinear behavior of CFRP axially stiffened panel under combined axial compression and torque</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Composite panel: shear buckling (left), pressure buckling (center) and composite strain (right)</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling modes in in axially compressed stiffened panel</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of a typical wing panel under axial compression</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_116.html"><img src="thumbnails/s116.jpg" width="103" height="180" border="0" hspace="14" vspace="0" alt="Buckling of an axially compressed, stringer-stiffened panel: finite element model and test"></a></td> <td width="208"><a href="pages/page_117.html"><img src="thumbnails/s117.jpg" width="180" height="103" border="0" hspace="14" vspace="0" alt="Post-buckling response of a J-stiffened composite shear panel"></a></td> <td width="208"><a href="pages/page_118.html"><img src="thumbnails/s118.jpg" width="180" height="115" border="0" hspace="14" vspace="0" alt="Buckling of a longitudinally stiffened panel under in-plane shear loading"></a></td> <td width="208"><a href="pages/page_119.html"><img src="thumbnails/s119.jpg" width="180" height="55" border="0" hspace="14" vspace="0" alt="Basic types of grid-stiffened panels"></a></td> <td width="208"><a href="pages/page_120.html"><img src="thumbnails/s120.jpg" width="180" height="107" border="0" hspace="14" vspace="0" alt="Buckling modes of grid-stiffened shells"></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">Buckling of an axially compressed, stringer-stiffened panel: finite element model and test</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Post-buckling response of a J-stiffened composite shear panel</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of a longitudinally stiffened panel under in-plane shear loading</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Basic types of grid-stiffened panels</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling modes of grid-stiffened shells</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

stiffened cylindrical shells

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Sunday, December 27, 2020