<?xml version="1.0" encoding="ISO-8859-1"?><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">
<front>
<journal-meta>
<journal-id>0012-7353</journal-id>
<journal-title><![CDATA[DYNA]]></journal-title>
<abbrev-journal-title><![CDATA[Dyna rev.fac.nac.minas]]></abbrev-journal-title>
<issn>0012-7353</issn>
<publisher>
<publisher-name><![CDATA[Universidad Nacional de Colombia]]></publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id>S0012-73532014000300009</article-id>
<title-group>
<article-title xml:lang="en"><![CDATA[Dynamic stability of slender columns with semi-rigid connections under periodic axial load: verification and examples]]></article-title>
<article-title xml:lang="es"><![CDATA[Estabilidad dinámica de columnas esbeltas con conexiones semirrígidas bajo carga axial periódica: verificación y ejemplos]]></article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Giraldo-Londoño]]></surname>
<given-names><![CDATA[Oliver]]></given-names>
</name>
<xref ref-type="aff" rid="A01"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Aristizábal-Ochoa]]></surname>
<given-names><![CDATA[J. Darío]]></given-names>
</name>
<xref ref-type="aff" rid="A02"/>
</contrib>
</contrib-group>
<aff id="A01">
<institution><![CDATA[,Ohio University  ]]></institution>
<addr-line><![CDATA[ ]]></addr-line>
<country>USA</country>
</aff>
<aff id="A02">
<institution><![CDATA[,National University School of Mines ]]></institution>
<addr-line><![CDATA[Medellin ]]></addr-line>
<country>Colombia</country>
</aff>
<pub-date pub-type="pub">
<day>00</day>
<month>06</month>
<year>2014</year>
</pub-date>
<pub-date pub-type="epub">
<day>00</day>
<month>06</month>
<year>2014</year>
</pub-date>
<volume>81</volume>
<numero>185</numero>
<fpage>66</fpage>
<lpage>72</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_arttext&amp;pid=S0012-73532014000300009&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_abstract&amp;pid=S0012-73532014000300009&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_pdf&amp;pid=S0012-73532014000300009&amp;lng=en&amp;nrm=iso"></self-uri><abstract abstract-type="short" xml:lang="en"><p><![CDATA[The dynamic stability of an elastic prismatic slender column with semirigid connections at both ends of identical stiffness and with sidesway between the two ends totally inhibited, subject to parametric axial loads including the combined effects of rotary inertia and external damping was presented in a companion paper. Closed-form expressions that predict the dynamic instability regions of slender columns were developed by making use of Floquet's theory. The proposed equations are straightforward and simple to apply. The proposed solution is capable of capturing the phenomena of stability of columns under periodic axial loads using a single column element. The proposed method and corresponding equations can be used to investigate the effects of damping, rotary inertia and semirigid connections on the stability analysis of slender columns under periodically varying axial loads. Sensitivity studies are presented herein that show the effects of rotary inertia, damping and semirigid connections on the dynamic stability of columns under parametric axial loads. Analytical studies indicate that the dynamic behavior of columns under periodic loading is strongly affected by the flexural stiffness of the end connections and the external damping, but not so much by the rotary inertia. Three examples are presented in detail and the calculated results are compared with those reported by other researchers.]]></p></abstract>
<abstract abstract-type="short" xml:lang="es"><p><![CDATA[La estabilidad dinámica de una columna elástica prismática esbelta con conexiones semirrígidas en ambos extremos de rigidez idéntica y con desplazamiento lateral entre los dos extremos totalmente inhibido sujetos a cargas axiales paramétricas incluyendo los efectos combinados de inercia rotacional y amortiguación externas fue presentada en una publicación adjunta. Expresiones cerradas que se pueden utilizar para predecir las regiones inestabilidad dinámica de columnas esbeltas se desarrollan haciendo uso de la teoría de Floquet. Las ecuaciones propuestas son sencillas y fáciles de aplicar. La solución propuesta es capaz de capturar el fenómeno de estabilidad en columnas sometidas a cargas axiales periódicas utilizando un solo elemento de columna. El método propuesto y las ecuaciones correspondientes se pueden utilizar para investigar los efectos del amortiguamiento, la inercia rotacional de la columna, y las conexiones semirrígidas en el análisis de estabilidad de columnas esbeltas sometidas a cargas axiales periódicas. Estudios de sensibilidad presentados en esta publicación muestran los efectos de la inercia rotacional, el amortiguamiento y las conexiones semi-rígidas en la estabilidad dinámica de columnas sometidas a cargas axiales paramétricas. Los estudios analíticos indican que el comportamiento dinámico de columnas bajo carga periódica está fuertemente afectado por la rigidez a la flexión de las conexiones de los dos apoyos y por el amortiguamiento externo, pero no tanto por la inercia rotacional. Tres ejemplos se presentan en detalle y los resultados calculados se comparan con los reportados por otros investigadores.]]></p></abstract>
<kwd-group>
<kwd lng="en"><![CDATA[Buckling]]></kwd>
<kwd lng="en"><![CDATA[Columns]]></kwd>
<kwd lng="en"><![CDATA[Dynamic Analysis]]></kwd>
<kwd lng="en"><![CDATA[Damping]]></kwd>
<kwd lng="en"><![CDATA[Semi-Rigid Connections]]></kwd>
<kwd lng="en"><![CDATA[Parametric Loading]]></kwd>
<kwd lng="en"><![CDATA[Periodic Loading]]></kwd>
<kwd lng="en"><![CDATA[Stability]]></kwd>
<kwd lng="es"><![CDATA[pandeo]]></kwd>
<kwd lng="es"><![CDATA[columnas]]></kwd>
<kwd lng="es"><![CDATA[análisis dinámico amortiguado]]></kwd>
<kwd lng="es"><![CDATA[conexiones semirígidas]]></kwd>
<kwd lng="es"><![CDATA[cargas paramétricas]]></kwd>
<kwd lng="es"><![CDATA[cargas periódicas]]></kwd>
<kwd lng="es"><![CDATA[estabilidad]]></kwd>
</kwd-group>
</article-meta>
</front><body><![CDATA[ <p align="left"><a href="http://dx.doi.org/10.15446/dyna.v81n185.36039" target="_blank">http://dx.doi.org/10.15446/dyna.v81n185.36039</a></p>      <p align="center"><font size="4" face="Verdana"><b>Dynamic stability of  slender columns with semi-rigid connections under periodic axial load: verification  and examples</b></font></p>     <p align="center"><i><font size="3"><b><font face="Verdana">Estabilidad  din&aacute;mica de columnas esbeltas con conexiones semirr&iacute;gidas bajo carga axial  peri&oacute;dica: verificaci&oacute;n y ejemplos</font></b></font></i></p>     <p align="center">&nbsp;</p>     <p align="center"><b><font size="2" face="Verdana">Oliver Giraldo-Londo&ntilde;o<sup> a</sup> &amp; J. Dar&iacute;o Aristiz&aacute;bal-Ochoa <sup>b</sup></font></b><font size="2" face="Verdana"></font></p>     <p align="center">&nbsp;</p>     <p align="center"><font size="2" face="Verdana"><sup><i>a </i></sup><i>Structural Researcher, M.S. Ohio University,  USA <a href="mailto:ogirald86@gmail.com">ogirald86@gmail.com</a>.    <br>  <sup>b </sup>125-Year Generation Professor, Ph.D. School of  Mines, National University. Medellin, Colombia <a href="mailto:jdaristi@unal.edu.co">jdaristi@unal.edu.co</a></i></font></p>     <p align="center">&nbsp;</p>     <p align="center"><font size="2" face="Verdana"><b>Received: December 15<sup>th</sup>, de 2012. Received in revised  form: December 20<sup>th</sup>, 2013. Accepted:  December 26<sup>th</sup>, 2013.</b></font></p>     ]]></body>
<body><![CDATA[<p>&nbsp;</p> <hr>     <p><font size="2" face="Verdana"><b>Abstract    <br>  </b></font><font size="2" face="Verdana">The dynamic stability  of an elastic prismatic slender column with semirigid connections at both ends  of identical stiffness and with sidesway between the two ends totally  inhibited, subject to parametric axial loads including the combined effects of  rotary inertia and external damping was presented in a companion paper.  Closed-form expressions that predict the dynamic instability regions of slender  columns were developed by making use of Floquet's theory. The proposed  equations are straightforward and simple to apply. The proposed solution is  capable of capturing the phenomena of stability of columns under periodic axial  loads using a single column element. The proposed method and corresponding  equations can be used to investigate the effects of damping, rotary inertia and  semirigid connections on the stability analysis of slender columns under  periodically varying axial loads. Sensitivity studies are presented herein that  show the effects of rotary inertia, damping and semirigid connections on the  dynamic stability of columns under parametric axial loads. Analytical studies  indicate that the dynamic behavior of columns under periodic loading is  strongly affected by the flexural stiffness of the end connections and the  external damping, but not so much by the rotary inertia. Three examples are  presented in detail and the calculated results are compared with those reported  by other researchers.</font></p>     <p><font size="2" face="Verdana"><i>Keywords:</i> Buckling, Columns, Dynamic Analysis, Damping, Semi-Rigid Connections,  Parametric Loading, Periodic Loading. Stability.</font></p>     <p><font size="2" face="Verdana"><b>Resumen    <br>  </b></font><font size="2" face="Verdana">La estabilidad din&aacute;mica de una columna el&aacute;stica prism&aacute;tica esbelta con  conexiones semirr&iacute;gidas en ambos extremos de rigidez id&eacute;ntica y con  desplazamiento lateral entre los dos extremos totalmente inhibido sujetos a  cargas axiales param&eacute;tricas incluyendo los efectos combinados de inercia  rotacional y amortiguaci&oacute;n externas fue presentada en una publicaci&oacute;n adjunta.  Expresiones cerradas que se pueden utilizar para predecir las regiones  inestabilidad din&aacute;mica de columnas esbeltas se desarrollan haciendo uso de la  teor&iacute;a de Floquet. Las ecuaciones propuestas son sencillas y f&aacute;ciles de  aplicar. La soluci&oacute;n propuesta es capaz de capturar el fen&oacute;meno de estabilidad  en columnas sometidas a cargas axiales peri&oacute;dicas utilizando un solo elemento  de columna. El m&eacute;todo propuesto y las ecuaciones correspondientes se pueden  utilizar para investigar los efectos del amortiguamiento, la inercia rotacional  de la columna, y las conexiones semirr&iacute;gidas en el an&aacute;lisis de estabilidad de  columnas esbeltas sometidas a cargas axiales peri&oacute;dicas. Estudios de  sensibilidad presentados en esta publicaci&oacute;n muestran los efectos de la inercia  rotacional, el amortiguamiento y las conexiones semi-r&iacute;gidas en la estabilidad  din&aacute;mica de columnas sometidas a cargas axiales param&eacute;tricas. Los estudios  anal&iacute;ticos indican que el comportamiento din&aacute;mico de columnas bajo carga  peri&oacute;dica est&aacute; fuertemente afectado por la rigidez a la flexi&oacute;n de las  conexiones de los dos apoyos y por el amortiguamiento externo, pero no tanto  por la inercia rotacional. Tres ejemplos se presentan en detalle y los  resultados calculados se comparan con los reportados por otros investigadores.</font></p>     <p><font size="2" face="Verdana"><i>Palabras claves:</i> pandeo, columnas,  an&aacute;lisis din&aacute;mico amortiguado, conexiones semir&iacute;gidas, cargas param&eacute;tricas,  cargas peri&oacute;dicas, estabilidad.</font></p> <hr>     <p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>1. Introduction</b></font></p>     <p><font size="2" face="Verdana">The main objective of this paper is to present examples  and sensitivity studies to verify an analytical method and closed-form  equations presented in a companion paper that determine the dynamic stability  of an elastic 2D prismatic column with semirigid connections with sidesway  between the two ends totally inhibited, subject to parametric axial load  described by a Fourier series. The proposed model and corresponding equations  which are straightforward and relatively simple to apply can be used to investigate  the effects of damping, rotary inertia and semirigid connections on the  stability of slender columns under periodically varying axial loads using a  single column element. The closed-form equations make use of Floquet's theory  to predict the dynamic instability regions of slender columns. Sensitivity  studies and three verification examples are included in this paper that shows  the effects of rotary inertia, damping and semirigid connections on the dynamic  stability of prismatic columns under parametric axial loads.</font></p>     ]]></body>
<body><![CDATA[<p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>2. Sensitivity  study</b></font></p>     <p><b><font size="2" face="Verdana">2.1. Dynamic Instability Regions for Damped Columns  Subjected to Harmonically Varying Axial Loads    <br>  </font></b><font size="2" face="Verdana">In this section closed-form expressions are developed that  determine the first two instability border lines for columns subjected to  periodic loads given by<sub><img src="img/revistas/dyna/v81n185/v81n185a09eq002.gif"></sub>.</font></p>     <p><font size="2" face="Verdana">Knowing the values of <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq004.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq006.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq008.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq010.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq012.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq014.gif"></sub> and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq016.gif"></sub> the non-dimensional  parameters, discussed in step (4) of the companion paper, can be calculated. In  this particular case the normalized axial load is written as <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq018.gif"></sub>, where: <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq020.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq0222.gif"></sub>, and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq024.gif"></sub>. This would correspond to <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq026.gif"></sub> with <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq028.gif"></sub>; <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq030.gif"></sub> (with <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq032.gif"></sub>); <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq034.gif"></sub>; and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq036.gif"></sub> (with <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq038.gif"></sub>). To determine the instability border lines, solutions with  period <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq040.gif"></sub> and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq0422.gif"></sub>must be considered.</font></p>     <p><font size="2" face="Verdana">The closed-form expression for the region of instability  corresponding to the solution with period <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq042.gif"></sub> can be found by  substituting the corresponding values of <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq044.gif"></sub>; <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq046.gif"></sub>, and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq048.gif"></sub> into Eq. (9) presented  in the companion paper as follows:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a09eq01.gif"></p>     <p><font size="2" face="Verdana">Now consider the solution with period <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq040.gif"></sub>. The closed-form expression for the instability region is  obtained by substituting the corresponding values of <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq044.gif"></sub>; <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq046.gif"></sub>, and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq048.gif"></sub> into Eq. (10)  presented in the companion paper as follows:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a09eq02.gif"></p>     <p><font size="2" face="Verdana">Sensitivity studies for different values of the damping  parameter, rotary inertia parameter, and fixity factor are carried out. <a href="#fig01">Fig. 1</a> shows the effect of damping in the dynamic instability regions taking <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq061.gif"> </sub>and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq063.gif"></sub> (or<sub><img src="img/revistas/dyna/v81n185/v81n185a09eq065.gif"></sub>) in Eqs. (1) and (2). Numerical results indicate that by increasing  the damping, the region of instability moves from left to right acquiring some  curvature as reported by Svensson &#91;2&#93; and Timoshenko and Gere &#91;3&#93;. <a href="#fig04">Fig. 4</a> shows  the variation of the region of instability corresponding to Eq. (1) for  different values of slenderness parameter. The effects of the stiffness of the  end connections on the instability regions are shown in <a href="#fig05">Fig. 5</a>.</font></p>     ]]></body>
<body><![CDATA[<p align="center"><font size="2" face="Verdana"><a name="fig01"></a></font><img src="img/revistas/dyna/v81n185/v81n185a09fig01.gif"></p>     <p><font size="2" face="Verdana"><a href="#fig02">Fig. 2</a> and <a href="#fig03">3</a> indicate that: 1) the effects of rotary  inertia on the dynamic response of slender columns subject to periodic axial  loads are negligible for reasonable values of slenderness; and 2) the dynamic  instability of a slender column subject to a periodic loading is greatly  affected by the stiffness of the end connections.</font></p>     <p align="center"><font size="2" face="Verdana"><a name="fig02"></a></font><img src="img/revistas/dyna/v81n185/v81n185a09fig02.gif"></p>     <p align="center"><font size="2" face="Verdana"><a name="fig03"></a></font><img src="img/revistas/dyna/v81n185/v81n185a09fig03.gif"></p>     <p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>3. Comprehensive  examples and verification</b></font></p>     <p><font size="2" face="Verdana"><b><i>Example 1:</i> <i>Column with Semi-rigid  Connections subjected to Rectified Sine Axial Load</i></b></font></p>     <p><font size="2" face="Verdana">Determine the stability regions for a damped column  elastically connected at both ends, given that: 1) the fixity factor of the  connections are: <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq063.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq102.gif"></sub>,<sub><img src="img/revistas/dyna/v81n185/v81n185a09eq097.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq105.gif"></sub>, and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq107.gif"></sub>; 2) the damping parameter is <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq109.gif"></sub>; and 3) the applied axial load is given by a rectified sine  wave as shown in <a href="#fig04">Fig. 4</a>.</font></p>     <p align="center"><font size="2" face="Verdana"><a name="fig04"></a></font><img src="img/revistas/dyna/v81n185/v81n185a09fig04.gif"></p>     <p><font size="2" face="Verdana"><b>Solution:</b> The first necessary step to carry out the dynamic  analysis of a slender column with semirigid connections is to determine the  parameter <img src="img/revistas/dyna/v81n185/v81n185a09eq113.gif">, which depends only of the fixity factor <img src="img/revistas/dyna/v81n185/v81n185a09eq115.gif">. By solving numerically Eq. 7b the values obtained are: <img src="img/revistas/dyna/v81n185/v81n185a09eq117.gif">,<img src="img/revistas/dyna/v81n185/v81n185a09eq119.gif">, <img src="img/revistas/dyna/v81n185/v81n185a09eq121.gif">, <img src="img/revistas/dyna/v81n185/v81n185a09eq123.gif">, and <img src="img/revistas/dyna/v81n185/v81n185a09eq125.gif">, for the respective values of the fixity factor. Now, to  evaluate the instability regions the expansion in Fourier series for the given  axial load must be known. The coefficients of the series are: <img src="img/revistas/dyna/v81n185/v81n185a09eq127.gif">, <img src="img/revistas/dyna/v81n185/v81n185a09eq129.gif">, <img src="img/revistas/dyna/v81n185/v81n185a09eq131.gif">. Closed expressions for the two first regions of instability  are obtained by substituting the values of <img src="img/revistas/dyna/v81n185/v81n185a09eq113.gif">, <img src="img/revistas/dyna/v81n185/v81n185a09eq133.gif">and the corresponding terms of the Fourier series into Eqs.  (9) and (10) presented in the companion paper.</font></p>     ]]></body>
<body><![CDATA[<p><font size="2" face="Verdana"><b><i>a)&nbsp;&nbsp;&nbsp;&nbsp; Solution with period </i>2<i>T</i></b></font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a09eq021.gif"></p>     <p><font size="2" face="Verdana"><b><i>b)&nbsp;&nbsp;&nbsp;&nbsp; Solution with period T</i></b></font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a09eq022.gif"></p>     <p><font size="2" face="Verdana"><a href="#fig05">Fig. 5</a> shows the two first regions of instability for the  prismatic column described above. Results indicate that under damping, regions  of instability move horizontally showing that a minimal value of the magnitude  of the applied axial load is necessary to make the system unstable. According  as the fixity factor of the connections increases, the minimal value of the  applied axial load also moves horizontally. As the connection becomes stiffer,  results also show that the principal region becomes narrower.</font></p>     <p align="center"><font size="2" face="Verdana"><a name="fig05"></a></font><img src="img/revistas/dyna/v81n185/v81n185a09fig05.gif"></p>     <p>&nbsp;</p>     <p><font size="2" face="Verdana"><b><i>EXAMPLE 2</i></b><i>: <b>Dynamic stability regions of a  hinged-hinged column under periodic loading</b></i></font></p>     <p><font size="2" face="Verdana">Determine the stability limits for a perfectly  hinged-hinged steel column. Assume that: it has a 1mmx25mm rectangular cross  section, <i>L</i>= 400 mm, and the applied  axial load<sub><img src="img/revistas/dyna/v81n185/v81n185a09eq145.gif"></sub>. Compare the results using the proposed method with those  reported by Svensson &#91;2&#93;. Neglect the effects of damping.</font></p>     <p><font size="2" face="Verdana"><b><i><u>Solution</u></i></b><i>:</i> Note that the values of <i>E</i>,<i> I</i>,<i> A</i>,<i> r</i>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq012.gif"></sub>are known, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq063.gif"></sub> (hinged at both ends), <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq113.gif"></sub>= 1 and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq133.gif"></sub>= 0 (damping effects are neglected). </font></p>     ]]></body>
<body><![CDATA[<p><font size="2" face="Verdana">From step (4) the normalized function <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq149.gif"></sub> can be written as <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq151.gif"></sub> with <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq153.gif"></sub>. Therefore for the expression <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq155.gif"></sub> to be satisfied, then<sub><img src="img/revistas/dyna/v81n185/v81n185a09eq157.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq159.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq161.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq163.gif"></sub>, and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq036.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq038.gif"></sub></font></p>     <p><font size="2" face="Verdana">Closed expressions for the first two regions of  instability are obtained by substituting <i>p= </i>0,<sub><img src="img/revistas/dyna/v81n185/v81n185a09eq065.gif"></sub>, and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq166.gif"></sub> into Eqs. (12) and  (13). Therefore:</font></p>     <p><font size="2" face="Verdana"><b><i>a)&nbsp;&nbsp;&nbsp;&nbsp; Solution with period 2T</i></b></font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a09eq03.gif"></p>     <p><font size="2" face="Verdana"><b><i>b)&nbsp;&nbsp;&nbsp;&nbsp; Solution with period T</i></b></font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a09eq04.gif"></p>     <p><font size="2" face="Verdana">The first two stability regions can be found simply by  increasing the values of <i>s </i>from zero  to 1 and plotting the four roots obtained from Eqs. (3) and (4). <a href="#fig06">Fig. 6</a> shows  these regions and the results are in accordance with those calculated and  reported by Svensson &#91;2&#93;. His experimental results are also shown.</font></p>     <p align="center"><font size="2" face="Verdana"><a name="fig06"></a></font><img src="img/revistas/dyna/v81n185/v81n185a09fig06.gif"></p>     <p><font size="2" face="Verdana"><b><i>Example 3</i></b><i>: <b>Pinned-Pinned column subjected  to saw-tooth Axial Load</b></i></font></p>     <p><font size="2" face="Verdana">A slender column subject to a saw-tooth periodic axial  load described by Kumar and Mohammed &#91;4&#93; is considered. The periodic load is  defined by case 4 listed in Table 1 of the companion paper. The corresponding  Fourier coefficients are: <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq199.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq036.gif"></sub>, and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq202.gif"></sub>. Assume that: <i>L= </i>7  m<i>, E=</i>2.1x10<sup>11 </sup>Pa<i> and I=</i>2.003x10<sup>-5</sup>m<sup>4</sup>.</font></p>     ]]></body>
<body><![CDATA[<p><font size="2" face="Verdana">Notice that:<sub><img src="img/revistas/dyna/v81n185/v81n185a09eq063.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq113.gif"></sub>= 1, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq133.gif"></sub>= 0 and <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq206.gif"></sub>= 1 (since the effect of rotary inertia is neglected). Thus,  the following equations for the two first regions of instability can be  obtained:</font></p>     <p><font size="2" face="Verdana"><b><i>a)&nbsp;&nbsp;&nbsp;&nbsp; Solution with period <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq042.gif"></sub></i></b></font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a09eq041.gif"></p>     <p align="center"><font size="2" face="Verdana"><a name="fig07"></a></font><img src="img/revistas/dyna/v81n185/v81n185a09fig07.gif"></p>     <p><font size="2" face="Verdana"><b><i>b)&nbsp;&nbsp;&nbsp;&nbsp; Solution with period <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq040.gif"></sub></i></b></font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a09eq042.gif"></p>     <p><font size="2" face="Verdana">Fig. 7 shows the principal region of instability that  corresponds to the solution with period <i>2T.</i> It can be seen that the obtained results using the proposed method are  practically identical to those reported by Kumar and Mohammed &#91;4&#93; obtained  using the FEM</font></p>     <p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>4. Summary and  conclusions </b></font></p>     <p><font size="2" face="Verdana">Closed-form expressions that can be used to predict the  dynamic instability regions of slender Euler-Bernoulli columns were developed  in a companion paper using Floquet's theory. The proposed method is  straightforward and the corresponding equations are relatively easy to use. The  proposed closed-form equations enable the analyst to explicitly evaluate the  effects of damping, semirigid connections, and rotary inertia on the nonlinear  elastic response and lateral stability of slender prismatic columns with  sidesway inhibited subject to static and dynamic axial loads. The proposed  equations are not available in the technical literature. A sensitivity study  and three examples are presented in detail that illustrate how to analyze the  dynamic stability of slender prismatic columns with sidesway totally inhibited  as the frequency and magnitude of the axial load varies.</font></p>     ]]></body>
<body><![CDATA[<p><font size="2" face="Verdana">Analytical results and sensitivity studies indicate that  the second-order dynamic response of a slender Euler-Bernoulli column subject  to periodic axial loads is affected by the rotary inertia, external damping,  and the stiffness of the end connections. It was found that for slender columns  the effects of rotary inertia are not as strong as those produced by damping  and the stiffness of the end connections. Analytical results indicate that: 1)  instability border lines move horizontally and acquire some curvature as the  damping increases; 2) as the stiffness of the end connections increases, the  frequencie of the applied axial load defining the instability border lines also  increase; and 3) the column axial deflection in the instability regions  decreases significantly as the fixity factor <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq115.gif"></sub> varies from zero (i.e.  for perfectly pinned-pinned columns) to one (i.e. for perfectly clamped-clamped  columns). These results are in accordance with those reported by other  researchers.</font></p>     <p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>Acknowledgments </b></font></p>     <p><font size="2" face="Verdana">The authors wish to thank the Department of Civil  Engineeering of the School of Mines of the National University of Colombia at  Medell&iacute;n and to COLCIENCIAS for their financial support.</font></p>     <p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>Notation</b></font></p>     <p><font size="2" face="Verdana">The following symbols are used in  both this paper and the companion paper:</font></p>     <p><font size="2" face="Verdana"><i>A</i> = area of the column cross section;    <br>  </font><font size="2" face="Verdana"><sub><img src="img/revistas/dyna/v81n185/v81n185a09eq216.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq218.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq220.gif"></sub>= coefficients of Fourier series utilized to describe the  applied axial load;    <br>  </font><font size="2" face="Verdana"><sub><img src="img/revistas/dyna/v81n185/v81n185a09eq222.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq224.gif"></sub>= constants;    ]]></body>
<body><![CDATA[<br>  </font><font size="2" face="Verdana"><i>c </i>= Damping coefficient;    <br>  </font><font size="2" face="Verdana"><sub><img src="img/revistas/dyna/v81n185/v81n185a09eq046.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq227.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq229.gif"></sub>= dimensionless coefficients of Fourier series utilized to  describe the applied axial load;    <br>  </font><font size="2" face="Verdana"><i>E</i> = Young's modulus of the material;    <br>  </font><font size="2" face="Verdana"><i>f</i>(<i>t</i>) = Amplification  function for lateral deflection of the column;    <br>  </font><font size="2" face="Verdana"><i>I</i> = Principal moment of inertia about its plane of bending of the  column;    <br>  </font><font size="2" face="Verdana"><i>L</i> = Column span;    <br>  </font><font size="2" face="Verdana"><i>M </i>= Bending moment along the column;    <br>  </font><font size="2" face="Verdana"><sub><img src="img/revistas/dyna/v81n185/v81n185a09eq231.gif"></sub>= Uniform mass per unit of length of the column (including  any additional uniformly distributed mass);    <br>  </font><font size="2" face="Verdana"><i>P</i>(<i>t</i>) = Periodic axial  load applied at the ends of the column;    <br>  </font><font size="2" face="Verdana"><i>p</i>(<i>t</i>) = Dimensionless  axial load;    ]]></body>
<body><![CDATA[<br>  </font><font size="2" face="Verdana"><i>r </i>= Radius of gyration of the column cross section;    <br>  </font><font size="2" face="Verdana"><i>R </i>= Slenderness parameter;    <br>  </font><font size="2" face="Verdana"><i>V</i> = Shear force;    <br>  </font><font size="2" face="Verdana"><i>y</i>(<i>x</i>, <i>t</i>) = Column lateral  deflection;    <br>  </font><font size="2" face="Verdana"><i>a </i>= Parameter used to  describe the shape function of the column;    <br>  </font><font size="2" face="Verdana"><i>k </i>= Stiffness of the  rotational restraint at both ends of the column;    <br>  </font><font size="2" face="Verdana"><i><sub><img src="img/revistas/dyna/v81n185/v81n185a09eq233.gif"></sub></i>= Angular frequency of the applied axial load;    <br>  </font><font size="2" face="Verdana"><i><sub><img src="img/revistas/dyna/v81n185/v81n185a09eq235.gif"></sub></i>= Angular frequency of the applied axial load  normalized with respect to <sub><img src="img/revistas/dyna/v81n185/v81n185a09eq237.gif"></sub>;    <br>  </font><font size="2" face="Verdana"><i>r </i>= Fixity factor at the  ends <i>A'</i> and <i>B'</i> of the column;    <br>  </font><font size="2" face="Verdana"><i>q</i> = Rotation of the cross  section due to bending;    ]]></body>
<body><![CDATA[<br>  </font><font size="2" face="Verdana"><i>t</i> = Dimensionless time  parameter;    <br>  </font><font size="2" face="Verdana"><i>w</i><sub>0</sub> = Natural frequency of lateral vibration  of a simply supported beam without axial load;    <br>  </font><font size="2" face="Verdana"><sub><img src="img/revistas/dyna/v81n185/v81n185a09eq239.gif"></sub>= Dimensionless parameter;    <br>  </font><font size="2" face="Verdana"><i>z</i> = Dimensionless damping  parameter.</font></p>     <p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>References</b></font></p>     <!-- ref --><p> <font size="2" face="Verdana"><b>&#91;1&#93;</b> Giraldo-Londo&ntilde;o, O. and Aristizabal-Ochoa, J. D., Dynamic stability of slender columns with semi-rigid connections under periodic axial load: Theory, Revista DYNA, accepted for publication, 2013.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000109&pid=S0012-7353201400030000900001&lng=','','width=640,height=500,resizable=yes,scrollbars=1,menubar=yes,');">Links</a>&#160;]<!-- end-ref --></font></p>     <!-- ref --><p> <font size="2" face="Verdana"><b>&#91;2&#93;</b> Svensson, I., Dynamic Instability regions in a Damped System, J. of Sound and Vibration, 244 (5), pp. 779-793, 2001.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000111&pid=S0012-7353201400030000900002&lng=','','width=640,height=500,resizable=yes,scrollbars=1,menubar=yes,');">Links</a>&#160;]<!-- end-ref --></font></p>     ]]></body>
<body><![CDATA[<!-- ref --><p> <font size="2" face="Verdana"><b>&#91;3&#93;</b> Timoshenko S. P. and Gere, J. M., Theory of Elastic Stability, 2nd Ed., McGraw-Hill Book Inc., New York, N.Y, 1961</font>&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000113&pid=S0012-7353201400030000900003&lng=','','width=640,height=500,resizable=yes,scrollbars=1,menubar=yes,');">Links</a>&#160;]<!-- end-ref --><!-- ref --><p> <font size="2" face="Verdana"><b>&#91;4&#93;</b> Kumar, T. H. and Mohammed A., Finite element analysis of dynamic stability of skeletal structures under periodic loading,&quot; J. of Zhejiang University SCIENCE A, Vol. 8 (2), 245-256, 2007. <a href="http://www.springerlink.com/content/e03352h0h1712153/" target="_blank">http://www.springerlink.com/content/e03352h0h1712153/</a> </font>     &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000114&pid=S0012-7353201400030000900004&lng=','','width=640,height=500,resizable=yes,scrollbars=1,menubar=yes,');">Links</a>&#160;]<!-- end-ref --><p>     <p><font size="2" face="Verdana"><b>Oliver Giraldo-Londo&ntilde;o </b>received the BS in Civil  Engineering in 2010 from Universidad Nacional de Colombia, Sede Medellin, and  the MS in Structural Engineering in 2014 from Ohio University at Athens, OH,  USA. From 2006-2009, he worked as undergraduate teacher assistant for the  department of mathematics at Universidad Nacional de Colombia, Sede Medellin.  From 2010-present, he has been working in the Structural Stability Research  Group (GES) at Universidad Nacional de Colombia, Sede Medellin, under the supervision  of Dr. J. Dario Aristizabal-Ochoa. From 2011-2012, he worked as instructor of  statics of structures and numerical methods at Universidad de Antioquia. From  2012-present, he has been working as graduate assistant at Ohio University at  Athens, OH, USA. He was awarded the Emilio Robledo award (Colombian Society of  Engineers, 2009) and the Young Researcher award (COLCIENCIAS, 2010-2011). Also,  he was COLFUTURO scholar (2012-2014). His research interests include analysis  and design of steel and concrete structures, non-linear mechanics, finite  element modeling, bridge engineering, earthquake engineering, and structural  dynamics.</font></p>     <p><font size="2" face="Verdana"><b>J. Dario Aristizabal-Ochoa, </b>received the  Bachelor degree in Civil Engineering in 1970 with honors from the National  University of Colombia. Medellin, Colombia, the MS and PhD degrees in  Structural Engineering in 1973 and 1976, respectively from the University of  Illinois at Champaign&#150;Urbana, USA. From 1977 to 1978, he worked for the  Portland Cement Association, Skokie, Illinois, USA as Structural Researcher.  From 1978-1981 he worked as Marketing Manager of Seismic Applications for MTS  Systems at Eden Prairie, Minnessota, USA. From 1981-1995 as Professor for the  Universities of Vanderbilt at Nashville, Tennessee and for the California State  University at Fullerton California, USA. Currently, he is full Professor and  director of the Structural Stability Research Group at the National University  of Colombia at Medellin. He was awarded the &quot;Engineering Foundation&quot; grant in  1982 by the American Institute of Civil Engineers (ASCE), the&nbsp;Raymond  Reese Structural award by the American Concrete Institute (ACI) in 1984, and two  NSF research grants in 1988 and 1989. Currently, he is a Full Professor in  Civil Engineering, School of Mines, and National University of Colombia at  Medellin. He is an active editorial member and reviewer of several  international Journals (ICE, ASCE, ACI, PCI, ELSEVIER, etc). His research  interests include: steel, reinforced concrete structures, structural dynamics  and stability, composite materials, analysis and design of bridges, nonlinear  analysis, seismic design, soil-structural interaction. His research work is  referenced by numerous textbooks and construction codes (ACI, AISC, ASSHTO) and  technical papers.</font></p>      ]]></body><back>
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<person-group person-group-type="author">
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<surname><![CDATA[Giraldo-Londoño]]></surname>
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<article-title xml:lang="en"><![CDATA[Dynamic stability of slender columns with semi-rigid connections under periodic axial load: Theory]]></article-title>
<source><![CDATA[Revista DYNA]]></source>
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<article-title xml:lang="en"><![CDATA[Dynamic Instability regions in a Damped System]]></article-title>
<source><![CDATA[J. of Sound and Vibration]]></source>
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<source><![CDATA[Theory of Elastic Stability]]></source>
<year>1961</year>
<edition>2nd Ed.</edition>
<publisher-loc><![CDATA[New York^eN.Y N.Y]]></publisher-loc>
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</person-group>
<article-title xml:lang="en"><![CDATA[Finite element analysis of dynamic stability of skeletal structures under periodic loading]]></article-title>
<source><![CDATA[J. of Zhejiang University SCIENCE A]]></source>
<year>2007</year>
<volume>8</volume>
<numero>2</numero>
<issue>2</issue>
<page-range>245-256</page-range></nlm-citation>
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</article>
