<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_1.html"><img src="thumbnails/s1.jpg" width="180" height="169" border="0" hspace="14" vspace="0" alt="Various cylindrical shells possibly with the same Batdorf parameter, Z"></a></td> <td width="208"><a href="pages/page_2.html"><img src="thumbnails/s2.jpg" width="180" height="168" border="0" hspace="14" vspace="0" alt="Linear buckling coefficients k from tests and theory for cylindrical shells under axial compression, torsion and external pressure"></a></td> <td width="208"><a href="pages/page_3.html"><img src="thumbnails/s3.jpg" width="180" height="143" border="0" hspace="14" vspace="0" alt="Industrial revolution meets space age: A circa 1965 device at the California Institute of Technology for testing cylindrical shells under axial compression"></a></td> <td width="208"><a href="pages/page_4.html"><img src="thumbnails/s4.jpg" width="180" height="62" border="0" hspace="14" vspace="0" alt="(a) Pre-buckling and (b,c) bifurcation buckling modes of uniformly axially compressed cylindrical shell"></a></td> <td width="208"><a href="pages/page_5.html"><img src="thumbnails/s5.jpg" width="150" height="180" border="0" hspace="14" vspace="0" alt="Plan views of typical bifurcation buckling modes of an axially compressed cylindrical shell. n is the number of full circumferential waves in the buckling mode."></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">Various cylindrical shells possibly with the same Batdorf parameter, Z</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Linear buckling coefficients k from tests and theory for cylindrical shells under axial compression, torsion and external pressure</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Industrial revolution meets space age: A circa 1965 device at the California Institute of Technology for testing cylindrical shells 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">(a) Pre-buckling and (b,c) bifurcation buckling modes of uniformly axially compressed cylindrical shell</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Plan views of typical bifurcation buckling modes of an axially compressed cylindrical shell. n is the number of full circumferential waves in the buckling mode.</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_6.html"><img src="thumbnails/s6.jpg" width="180" height="112" border="0" hspace="14" vspace="0" alt="Buckling of axially compressed cylindrical shell: buckling modes vs shell length"></a></td> <td width="208"><a href="pages/page_7.html"><img src="thumbnails/s7.jpg" width="180" height="83" border="0" hspace="14" vspace="0" alt="Three dimensional rendering of a typical buckling mode with 2 axial half-waves and 4 full circumferential waves"></a></td> <td width="208"><a href="pages/page_8.html"><img src="thumbnails/s8.jpg" width="180" height="155" border="0" hspace="14" vspace="0" alt="Buckling curves for axially compressed isotropic cylindrical shells"></a></td> <td width="208"><a href="pages/page_9.html"><img src="thumbnails/s9.jpg" width="180" height="142" border="0" hspace="14" vspace="0" alt=" Variation of critical stress in simply supported cylindrical shells from Donnell’s and Sanders’ theories (a=radius, n=circ.waves)"></a></td> <td width="208"><a href="pages/page_10.html"><img src="thumbnails/s10.jpg" width="180" height="178" border="0" hspace="14" vspace="0" alt="Buckled axially compressed 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">Buckling of axially compressed cylindrical shell: buckling modes vs shell length</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Three dimensional rendering of a typical buckling mode with 2 axial half-waves and 4 full circumferential waves</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling curves for axially compressed isotropic cylindrical shells</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title"> Variation of critical stress in simply supported cylindrical shells from Donnell’s and Sanders’ theories (a=radius, n=circ.waves)</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckled axially compressed 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_11.html"><img src="thumbnails/s11.jpg" width="124" height="180" border="0" hspace="14" vspace="0" alt="Buckled thin unstiffened axially compressed cylindrical shell"></a></td> <td width="208"><a href="pages/page_12.html"><img src="thumbnails/s12.jpg" width="180" height="103" border="0" hspace="14" vspace="0" alt=""Classical" buckling stress of a thin, monocoque, perfect, elastic, uniformly axially compressed cylindrical shell"></a></td> <td width="208"><a href="pages/page_13.html"><img src="thumbnails/s13.jpg" width="180" height="110" border="0" hspace="14" vspace="0" alt="Buckling of thin isotropic cylindrical shells under uniform axial compression"></a></td> <td width="208"><a href="pages/page_14.html"><img src="thumbnails/s14.jpg" width="180" height="118" border="0" hspace="14" vspace="0" alt="Comparison of test versus theory for buckling of axially compressed isotropic cylindrical shells"></a></td> <td width="208"><a href="pages/page_15.html"><img src="thumbnails/s15.jpg" width="180" height="111" border="0" hspace="14" vspace="0" alt="Comparison of test versus theory for buckling of axially compressed isotropic cylindrical 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">Buckled thin unstiffened axially compressed cylindrical shell</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">"Classical" buckling stress of a thin, monocoque, perfect, elastic, uniformly axially compressed cylindrical shell</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Buckling of thin isotropic cylindrical shells under uniform axial compression</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Comparison of test versus theory for buckling of axially compressed isotropic cylindrical shells</small></td></tr></table></td> <td width="208"><table cellspacing="0" cellpadding="5" border="0"><tr><td align="center"><small class="title">Comparison of test versus theory for buckling of axially compressed isotropic cylindrical shells</small></td></tr></table></td> </tr> <tr><td height="14"></td></tr> </table>

unstiffened cylindrical shells

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Sunday, December 27, 2020