<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_256.html"><img src="thumbnails/s256.jpg" width="180" height="81" border="0" hspace="14" vspace="0" alt="Preliminary 3D printed nacre-like composite prototypes of different shapes and material combinations."></a></td> <td width="208"><a href="pages/page_257.html"><img src="thumbnails/s257.jpg" width="180" height="140" border="0" hspace="14" vspace="0" alt="Multiscale simulation strategy in connection with composite materials used for aircraft"></a></td> <td width="208"><a href="pages/page_258.html"><img src="thumbnails/s258.jpg" width="180" height="116" border="0" hspace="14" vspace="0" alt="Elastic beam subjected to time-varying lateral distributed load q"></a></td> <td width="208"><a href="pages/page_259.html"><img src="thumbnails/s259.jpg" width="180" height="108" border="0" hspace="14" vspace="0" alt="Non-chaotic behavior of the beam for a low-amplitude load, q-sub-0 = 200"></a></td> <td width="208"><a href="pages/page_260.html"><img src="thumbnails/s260.jpg" width="180" height="111" border="0" hspace="14" vspace="0" alt="Partially chaotic behavior of the beam at the load amplitude, q-sub-0 = 1000"></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">Preliminary 3D printed nacre-like composite prototypes of different shapes and material combinations.</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Multiscale simulation strategy in connection with composite materials used for aircraft</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Elastic beam subjected to time-varying lateral distributed load q</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Non-chaotic behavior of the beam for a low-amplitude load, q-sub-0 = 200</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Partially chaotic behavior of the beam at the load amplitude, q-sub-0 = 1000</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_261.html"><img src="thumbnails/s261.jpg" width="180" height="112" border="0" hspace="14" vspace="0" alt="More chaotic behavior of the beam at the load amplitude, q-sub-0 = 39000"></a></td> <td width="208"><a href="pages/page_262.html"><img src="thumbnails/s262.jpg" width="144" height="180" border="0" hspace="14" vspace="0" alt="Axially compressed nonlinear dynamic behavior of a plate for two normalized loads Po = 4 and Po =8.25 "></a></td> <td width="208"><a href="pages/page_263.html"><img src="thumbnails/s263.jpg" width="180" height="137" border="0" hspace="14" vspace="0" alt="Nonlinear dynamic response of a locally transversely loaded shallow shell for 4 pairs (qo,omegap) of load amplitude qo and frequency omegap"></a></td> <td width="208"><a href="pages/page_264.html"><img src="thumbnails/s264.jpg" width="97" height="179" border="0" hspace="14" vspace="0" alt="Chaotic dynamic response of cylindrical shell with a transverse patch load, q = qosin(omegayt) "></a></td> <td width="208"><a href="pages/page_265.html"><img src="thumbnails/s265.jpg" width="143" height="180" border="0" hspace="14" vspace="0" alt="Shell vibration regimes including chaos"></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">More chaotic behavior of the beam at the load amplitude, q-sub-0 = 39000</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Axially compressed nonlinear dynamic behavior of a plate for two normalized loads Po = 4 and Po =8.25 </small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Nonlinear dynamic response of a locally transversely loaded shallow shell for 4 pairs (qo,omegap) of load amplitude qo and frequency omegap</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Chaotic dynamic response of cylindrical shell with a transverse patch load, q = qosin(omegayt) </small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Shell vibration regimes including chaos</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_266.html"><img src="thumbnails/s266.jpg" width="180" height="58" border="0" hspace="14" vspace="0" alt="Plan views of paired buckling modes of any closed isotropic shell of revolution"></a></td> <td width="208"><a href="pages/page_267.html"><img src="thumbnails/s267.jpg" width="159" height="180" border="0" hspace="14" vspace="0" alt="Substructuring of an airplane wing"></a></td> <td width="208"><a href="pages/page_268.html"><img src="thumbnails/s268.jpg" width="180" height="136" border="0" hspace="14" vspace="0" alt="Undeformed and deformed attice with (a) tension and (b) compression applied in the horizontal direction"></a></td> <td width="208"><a href="pages/page_269.html"><img src="thumbnails/s269.jpg" width="180" height="65" border="0" hspace="14" vspace="0" alt="Buckling and large deflection of thin band"></a></td> <td width="208"><a href="pages/page_270.html"><img src="thumbnails/s270.jpg" width="180" height="85" border="0" hspace="14" vspace="0" alt="Beam with actuator (bottom) and sensor (top) piezoelectric patches for controlling and sensing free vibration from a suddenly removed load at the tip"></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">Plan views of paired buckling modes of any closed isotropic shell of revolution</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Substructuring of an airplane wing</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Undeformed and deformed attice with (a) tension and (b) compression applied in the horizontal direction</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling and large deflection of thin band</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Beam with actuator (bottom) and sensor (top) piezoelectric patches for controlling and sensing free vibration from a suddenly removed load at the tip</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

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