<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_211.html"><img src="thumbnails/s211.jpg" width="180" height="78" border="0" hspace="14" vspace="0" alt="Effect of eccentrically oblique stiffeners and temperature on the nonlinear static and dynamic response of S-FGM cylindrical panels"></a></td> <td width="208"><a href="pages/page_212.html"><img src="thumbnails/s212.jpg" width="180" height="74" border="0" hspace="14" vspace="0" alt="Internally stiffened cylindrical shell subjected to an external explosion"></a></td> <td width="208"><a href="pages/page_213.html"><img src="thumbnails/s213.jpg" width="180" height="106" border="0" hspace="14" vspace="0" alt="Elements involved in the fuselage drop test"></a></td> <td width="208"><a href="pages/page_214.html"><img src="thumbnails/s214.jpg" width="180" height="81" border="0" hspace="14" vspace="0" alt="This is the test specimen"></a></td> <td width="208"><a href="pages/page_215.html"><img src="thumbnails/s215.jpg" width="180" height="115" border="0" hspace="14" vspace="0" alt="Getting ready for the fuselage drop test"></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">Effect of eccentrically oblique stiffeners and temperature on the nonlinear static and dynamic response of S-FGM cylindrical panels</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Internally stiffened cylindrical shell subjected to an external explosion</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Elements involved in the fuselage drop test</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">This is the test specimen</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Getting ready for the fuselage drop test</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_216.html"><img src="thumbnails/s216.jpg" width="180" height="85" border="0" hspace="14" vspace="0" alt="The fuselage section is dropped"></a></td> <td width="208"><a href="pages/page_217.html"><img src="thumbnails/s217.jpg" width="180" height="130" border="0" hspace="14" vspace="0" alt="The dropped fuselage is damaged"></a></td> <td width="208"><a href="pages/page_218.html"><img src="thumbnails/s218.jpg" width="180" height="115" border="0" hspace="14" vspace="0" alt="Axially compressed, dented, ring- and stringer-stiffened cylindrical shell"></a></td> <td width="208"><a href="pages/page_219.html"><img src="thumbnails/s219.jpg" width="180" height="94" border="0" hspace="14" vspace="0" alt="Vibrating stiffened cylindrical panel with resonators and foam"></a></td> <td width="208"><a href="pages/page_220.html"><img src="thumbnails/s220.jpg" width="177" height="180" border="0" hspace="14" vspace="0" alt="Reference design of a uniformly longitudinally compressed longitudinally stiffened plate in which the thickness of all parts is 1.27 mm"></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">The fuselage section is dropped</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">The dropped fuselage is damaged</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Axially compressed, dented, ring- and stringer-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">Vibrating stiffened cylindrical panel with resonators and foam</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Reference design of a uniformly longitudinally compressed longitudinally stiffened plate in which the thickness of all parts is 1.27 mm</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_221.html"><img src="thumbnails/s221.jpg" width="180" height="48" border="0" hspace="14" vspace="0" alt="Optimization of the longitudinally loaded and stiffened plate in which material voids and tapering of the stiffeners are permitted "></a></td> <td width="208"><a href="pages/page_222.html"><img src="thumbnails/s222.jpg" width="180" height="152" border="0" hspace="14" vspace="0" alt="Optimized design of the longitudinally loaded and stiffened plate"></a></td> <td width="208"><a href="pages/page_223.html"><img src="thumbnails/s223.jpg" width="180" height="87" border="0" hspace="14" vspace="0" alt="Modeling the effect of a stiffener fillet radius on the prediction of buckling under axial compression"></a></td> <td width="208"><a href="pages/page_224.html"><img src="thumbnails/s224.jpg" width="180" height="135" border="0" hspace="14" vspace="0" alt="Lattice cylindrical shell with elliptical cross section"></a></td> <td width="208"><a href="pages/page_225.html"><img src="thumbnails/s225.jpg" width="180" height="124" border="0" hspace="14" vspace="0" alt="Buckling of axially compressed lattice cylindrical shells with elliptical cross sections of various narrowness"></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">Optimization of the longitudinally loaded and stiffened plate in which material voids and tapering of the stiffeners are permitted </small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Optimized design of the longitudinally loaded and stiffened plate</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Modeling the effect of a stiffener fillet radius on the prediction of buckling under axial compression</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Lattice cylindrical shell with elliptical cross section</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of axially compressed lattice cylindrical shells with elliptical cross sections of various narrowness</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

stiffened cylindrical shells

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Sunday, December 27, 2020