<?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>S0012-73532014000300008</article-id>
<article-id pub-id-type="doi">10.15446/dyna.v81n185.36038</article-id>
<title-group>
<article-title xml:lang="en"><![CDATA[Dynamic stability of slender columns with semi-rigid connections under periodic axial load: theory]]></article-title>
<article-title xml:lang="es"><![CDATA[Estabilidad dinámica de columnas esbeltas con conexiones semirrígidas bajo carga axial periódica: teoría]]></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>56</fpage>
<lpage>65</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_arttext&amp;pid=S0012-73532014000300008&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_abstract&amp;pid=S0012-73532014000300008&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_pdf&amp;pid=S0012-73532014000300008&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 is investigated in a classical manner. Closed-form expressions that can be used to predict the dynamic instability regions of slender columns are developed by making use of Floquet's theory. 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. The effects produced by shear deformations along the span of the column as well as those produced by the axial inertia, the coupling between longitudinal and transverse deflections and the curvature are not taken into account. Sensitivity studies are presented in a companion paper that show the effects of rotary inertia, damping and semirigid connections on the dynamic stability of columns under parametric axial loads.]]></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 paramétricos incluyendo los efectos combinados de inercia rotacional y amortiguación externas se investiga de una manera clásica. Expresiones cerradas que se pueden utilizar para predecir las regiones de inestabilidad dinámica de columnas esbeltas son desarrolladas haciendo uso de la teoría de Floquet. 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. Los efectos producidos por las deformaciones por cizallamiento a lo largo de la columna, así como los producidos por la inercia axial, el acoplamiento entre las deflexiones longitudinales y transversales y la curvatura no se tienen en cuenta. Estudios de sensibilidad que 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 son presentados en una publicación adjunta.]]></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.v81n185.36038" target="_blank">http://dx.doi.org/10.15446/dyna.v81n185.36038</a></p>      <p align="center"><font size="4" face="Verdana"><b>Dynamic stability of slender columns with  semi-rigid connections under periodic axial load: theory</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: teor&iacute;a</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: September 26<sup>th</sup>, 2013. Accepted:  October 22<sup>th</sup>, 2013</b></font></p> <hr>     ]]></body>
<body><![CDATA[<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 is  investigated in a classical manner. Closed-form expressions that can be used to  predict the dynamic instability regions of slender columns are developed by  making use of Floquet's theory. 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. The effects produced by shear deformations along the span of the column  as well as those produced by the axial inertia, the coupling between  longitudinal and transverse deflections and the curvature are not taken into  account. Sensitivity studies are presented in a companion paper that show the  effects of rotary inertia, damping and semirigid connections on the dynamic  stability of columns under parametric axial loads. </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;tricos  incluyendo los efectos combinados de inercia rotacional y amortiguaci&oacute;n  externas se investiga de una manera cl&aacute;sica. Expresiones cerradas que se pueden  utilizar para predecir las regiones de inestabilidad din&aacute;mica de columnas  esbeltas son desarrolladas haciendo uso de la teor&iacute;a de Floquet. 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. Los efectos producidos por las  deformaciones por cizallamiento a lo largo de la columna, as&iacute; como los  producidos por la inercia axial, el acoplamiento entre las deflexiones longitudinales  y transversales y la curvatura no se tienen en cuenta. Estudios de sensibilidad  que 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 son presentados en una publicaci&oacute;n adjunta.</font></p>     <p><font size="2" face="Verdana"><i>Palabras clave:</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&nbsp; Introduction</b></font></p>     <p><font size="2" face="Verdana">The stability analysis of columns  and frames under time varying parametric axial loads are of great importance in  civil, mechanical, and aerospace engineering. This subject generally termed  &quot;Dynamic Stability&quot; has been investigated by numerous structural researchers  since Koning and Taub &#91;1&#93; studied the stability of a simply supported elastic  imperfect column subjected to a sudden applied axial load of known duration.  Dynamic Stability encompasses many classes of problems and many different  phenomena for the same configuration subjected to the same dynamic loads.  Therefore, it is not surprising that several uses and interpretations of the  term exist. Simitses and Hodges &#91;2&#93; on page 329 of their textbook state that:  &quot;The class of problems falling in the category of parametric excitation, or  parametric resonance, includes the best defined, conceived, and understood  problems of dynamic stability&quot;. The problem of parametric excitation is best  defined in terms of an example. Consider an Euler column, which is loaded at  one end by a periodic axial force. The other end is immovable. It can be shown  that, for certain relationships between the exciting frequency and the column  natural frequency of transverse vibration, transverse vibrations occur with  rapidly increasing amplitudes. This is called parametric resonance and the  system is said to be dynamically unstable. Moreover the loading is called  &quot;parametric excitation&quot;. Bolotin &#91;3&#93; is an excellent reference on Dynamic  Stability. Because of space limitation a brief bibliography of some studies  made in the last forty years is presented next.</font></p>     <p><font size="2" face="Verdana">Wirsching and Yao &#91;4&#93; developed a relationship for the  stability condition of a pin-ended column with initial curvature excited by  physical white noise. Iwatsubo et al. &#91;5&#93; studied the instabilities of a  cantilever column subject to an axial periodic load (Euler-type problem) and to  a tangential periodic load (Beck-type problem). Ahmadi and Glockner &#91;6&#93; studied  the stability of a viscous-elastic column subject to deterministic axial load  with sinusoidal time variation as well as stationary and non-stationary random  variations. Simitses &#91;7&#93; presented the concept of dynamic stability for  suddenly-loaded elastic structural configurations along the related criteria  and estimates of critical conditions. Sridharan and Benito &#91;8&#93; studied  experimentally the interaction of local and overall buckling in thin-walled  columns and the effect of suddenly applied compression dynamic end loads. Shigematsu  et al. &#91;9&#93; studied the dynamic stability of initially imperfect columns and  plates under time-dependent axial compression in elastic and elastic-plastic  regions using matrix functions.</font></p>     ]]></body>
<body><![CDATA[<p><font size="2" face="Verdana">Sophianopoulos and Kounadis &#91;10&#93;  studied the dynamic stability of imperfect frames under joint displacements.  Wong and Yang &#91;11&#93; studied the inelastic response of structures with  strain-hardening and strain-softening properties as well as with  elastic-plastic properties subjected to dynamic loadings using the force analogy  method. Svensson &#91;12&#93; studied theoretically and experimentally the stability of  a dynamic system with periodic coefficients including the effects of both  internal damping and damping at the boundaries.</font></p>     <p><font size="2" face="Verdana">Yabuki et al. &#91;13&#93; studied the inelastic dynamic stability  of steel columns subject to a steady axial force and an alternating dynamic  axial force including the effects of support conditions and the frequency of  the axial force. Kumar and Mohammed &#91;14&#93; studied the dynamic stability of  columns and frames subjected to axial periodic loads using the FEM and Newmark  method for the integration of the equations of motion. Dohnal et al. &#91;15&#93;  studied the behavior of a uniform cantilever column under a time-periodic axial  force using the FEM. Mailybaev and Seyranian &#91;16&#93; studied the classical problem  of stabilization of a statically unstable elastic column (simply supported and  clamped&#150;hinged ends) by axial harmonic vibration.</font></p>     <p><font size="2" face="Verdana">The main objective of this paper  is to present an analytical method and closed form equations that determine the  dynamic stability of an elastic 2D prismatic column with semirigid end  connections of identical stiffness and 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. Nonlinear effects like those  produced by the axial inertia, the coupling between longitudinal and transverse  deflections, and the curvature are not taken into account. Sensitivity studies  are included in a companion paper &#91;17&#93; that shows the effects of rotary inertia,  damping and semirigid connections on the dynamic stability of prismatic columns  under parametric axial loads.</font></p>     <p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>2&nbsp; Structural model</b></font></p>     <p><font size="2" face="Verdana">Consider the 2D prismatic column  elastically connected at both ends <i>A</i> and <i>B</i> as shown in <a href="#fig01">Fig. 1a</a>. The  element <i>AB</i> consists of the column  itself <i>A'B' </i>connected by elastic  springs <i>AA'</i> and <i>BB'</i> both with identical flexural stiffness <i>k</i> (whose dimension is force-distance/radian) at ends <i>A'</i> and <i>B'</i>, respectively.  It is assumed that the column <i>A'B'</i>:  (1) is prismatic with cross sectional area <i>A</i>,  principal moment of inertia <i>I</i> (about  the axis of bending), and span <i>L</i>; (2)  is made of a linear elastic, homogeneous and isotropic material with elastic  modulus <i>E</i>; (3) its initial centroidal  axis is a perfect straight line; (4) is subjected to a varying end axial load  defined by a Fourier series</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq000.gif"></p>     <p><font size="2" face="Verdana">as shown by <a href="#fig01">Fig. 1a</a>; and (5) bending deformations and  strains are small so that the principle of superposition can be applied.</font></p>     <p align="center"><font size="2" face="Verdana"><a name="fig01"></a></font><img src="img/revistas/dyna/v81n185/v81n185a08fig01.gif"></p>     <p><font size="2" face="Verdana">The ratio <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq006.gif"></sub>will be denoted as the stiffness index of the flexural  connections. The stiffness index varies from zero for perfectly pinned  connections to infinity for fully restrained connections (i.e., perfectly  clamped). For convenience the term <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq008.gif"></sub> denoted as the <i>fixity factor </i>is used in the proposed equations.</font></p>     ]]></body>
<body><![CDATA[<p><font size="2" face="Verdana"><b>2.1. Dynamic  Analysis    <br>  </b>The lateral  deflection of the column is derived by applying dynamic equilibrium on  the differential element (<a href="#fig01">Fig. 1b</a>) and compatibility conditions at the ends of  the member. The transverse and rotational dynamic equilibrium equations are:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq0102.gif"></p>     <p><font size="2" face="Verdana">Using the governing bending equation for Euler-Bernoulli  columns <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq014.gif"> </sub>and  substituting Eq. (1) into Eq. (2), the governing fourth-order differential  equation of a prismatic column becomes:</font></p> <img src="img/revistas/dyna/v81n185/v81n185a08eq03.gif">     <p><font size="2" face="Verdana">Equation (3) must meet the following four boundary  conditions:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq0405.gif"></p>     <p><font size="2" face="Verdana">The solution of Eq. (3) can be written in the following  form:</font></p> <img src="img/revistas/dyna/v81n185/v81n185a08eq06.gif">     <p><font size="2" face="Verdana"><sub> </sub>Where  the constant <i>a</i> must satisfy the following condition:</font></p> <img src="img/revistas/dyna/v81n185/v81n185a08eq071.gif">     <p><font size="2" face="Verdana">In terms of the fixity factor <i>r</i> Eq. (7a) becomes:</font></p> <img src="img/revistas/dyna/v81n185/v81n185a08eq072.gif">     <p><font size="2" face="Verdana">Equation (6) coupled with the condition given by Eq. (7b)  satisfies the four boundary conditions expressed by Eqs (4a-b) and (5a-b)  listed above. Substituting Eq. (6) into (3) the following ordinary differential  equation in <i>f</i>(<i>t</i>) is obtained:</font></p>     ]]></body>
<body><![CDATA[<p><img src="img/revistas/dyna/v81n185/v81n185a08eq081.gif"></p>     <p><font size="2" face="Verdana">To facilitate the analysis of columns subjected to varying  axial forces, the following six dimensionless parameters are introduced:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq0811.gif"></p>     <p><font size="2" face="Verdana">Where: <img src="img/revistas/dyna/v81n185/v81n185a08eq046.gif">= the natural frequency of lateral vibration of a simply  supported beam without axial load.</font></p>     <p><font size="2" face="Verdana">Then Eq. (8a) is reduced to</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq082.gif"></p>     <p><font size="2" face="Verdana"><b>2.2. Proposed  Equations for Instability Borders    <br>  </b></font><font size="2" face="Verdana">The proposed equations  are based on Floquet's theory. The derivation is presented in Appendix I for  easy reference.</font></p>     <p><font size="2" face="Verdana">As can be seen the character of the solutions for Eq. (8b)  depends on the values of its harmonically varying coefficients leading to  stable or unstable conditions. From Floquet's theory it can be concluded that  on the border between stable and unstable conditions the solutions for Eq. (8b)  becomes periodic with period <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq058.gif"></sub> or <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq060.gif"></sub> with <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq062.gif"></sub>.</font></p>     <p><font size="2" face="Verdana">The proposed equations shown below are capable to capture  the phenomena of parametric resonance of slender columns with semi rigid  connections, considering the effects of damping and rotary inertia:</font></p>     ]]></body>
<body><![CDATA[<p><font size="2" face="Verdana">a) Solution with period 2T</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq09.gif"></p>     <p><font size="2" face="Verdana">b) Solution with period T</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq10.gif"></p>     <p><font size="2" face="Verdana">where A, B and C are calculated as  indicated below.</font></p>     <p><font size="2" face="Verdana">When</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq101.gif"></p>     <p><font size="2" face="Verdana">When both <img src="img/revistas/dyna/v81n185/v81n185a08eq084.gif"> and <img src="img/revistas/dyna/v81n185/v81n185a08eq086.gif"> are different from  zero, Eq. (10) is not applicable and the solution shall be obtained by solving  Eq. (23b).</font></p>     <p><font size="2" face="Verdana"><a href="#tab01">Table 1</a> lists closed expressions for different classic  types of periodic axial loads. These expressions can be used to investigate the  effects of damping, rotary inertia and semirigid connections on the stability  of slender columns subject to periodic axial  loads in a systematic manner. For periodic loadings that are not listed in <a href="#tab01">Table 1</a>, simply use Eqs. (9) and (10) with the appropriate values of <img src="img/revistas/dyna/v81n185/v81n185a08eq084.gif"> and <img src="img/revistas/dyna/v81n185/v81n185a08eq086.gif">. shows graphically the two first regions of instability for  all types of loading described in <a href="#tab01">Table 1</a> by considering <img src="img/revistas/dyna/v81n185/v81n185a08eq090.gif"> (i.e. pinned-pinned  columns) and the corresponding values for <img src="img/revistas/dyna/v81n185/v81n185a08eq084.gif"> and <img src="img/revistas/dyna/v81n185/v81n185a08eq086.gif"> in Eqs. (9) and (10).</font></p>     <p align="center"><font size="2" face="Verdana"><a name="tab01"></a></font><img src="img/revistas/dyna/v81n185/v81n185a08tab01.gif"></p>     ]]></body>
<body><![CDATA[<p>&nbsp;</p>     <p><font size="3" face="Verdana"><b>3. Step-by-step  procedure</b></font></p>     <p><font size="2" face="Verdana">The following steps are proposed to evaluate the dynamic  stability for columns subjected to periodic axial loads:</font></p>     <p><font size="2" face="Verdana">1.&nbsp;&nbsp;&nbsp; Enter  the numerical values of the properties of the column:<sub><img src="img/revistas/dyna/v81n185/v81n185a08eq092.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq094.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq096.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq098.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq100.gif"></sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq1022.gif"></sub>, and <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq104.gif"></sub>.</font></p>     <p><font size="2" face="Verdana">2.&nbsp;&nbsp;&nbsp; With  the value of the flexural stiffness of the connection <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq106.gif"></sub> (or the fixity factor<sub><img src="img/revistas/dyna/v81n185/v81n185a08eq108.gif"></sub>), the value of the dimensionless parameter <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq110.gif"></sub> is calculated from Eq.  (7a) or (7b) using numerical methods (i.e., Newton-Raphson or secant method).  The values of <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq110.gif"></sub> must be between 1 and  2 for hinged and clamped in both ends, respectively, to obtain a coherent  solution to Eq. (6).</font></p>     <p><font size="2" face="Verdana">3.&nbsp;&nbsp;&nbsp; Calculate  the natural frequency of lateral vibration for a simple supported beam without  axial load:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq102.gif"></p>     <p><font size="2" face="Verdana">1.&nbsp;&nbsp;&nbsp; Determine the following  dimensionless parameters:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq103.gif"></p>     <p><font size="2" face="Verdana">2.&nbsp;&nbsp;&nbsp; To determine the borders  between regions of stability and instability Equations (9) and (10) must be used. Notice that the varying axial load  can be defined by the Fourier series</font></p>     ]]></body>
<body><![CDATA[<p><font size="2" face="Verdana"><sub><img src="img/revistas/dyna/v81n185/v81n185a08eq124.gif"></sub> with the terms <i>P</i><sub>0</sub>, <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq126.gif"></sub> and <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq128.gif"></sub> expressed by</font></p>     <p><font size="2" face="Verdana"><sub><img src="img/revistas/dyna/v81n185/v81n185a08eq130.gif"></sub>; <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq132.gif"></sub>; and <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq134.gif"></sub>. Where: <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq136.gif"></sub>. (with <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq138.gif"></sub>). The values of these parameters determine the stability  borders. Since the determination of the zeros of Eq. (16b) can become  cumbersome when both <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq084.gif"></sub> and <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq086.gif"></sub> are different from  zero, a numerical method similar to that used for solving Eq. (7a) or (7b) can  be used.</font></p>     <p><font size="2" face="Verdana">3.&nbsp;&nbsp;&nbsp; In order to estimate which  regions at both sides of the borders, obtained from step (5), are of stability  or instability is necessary to evaluate trial points located at both sides of  the borders, and evaluate the behavior of <img src="img/revistas/dyna/v81n185/v81n185a08eq140.gif"> by applying a  numerical method for solving the ordinary differential equations. The  Runge-Kutta method is suggested in this case since it is simple, efficient and  accurate. To describe how to solve Eq. (8b) using the Runge-Kutta method, the  system of ordinary differential equations defined by Eq. (16) is rewritten as  follows:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq11.gif"></p>     <p><font size="2" face="Verdana">The method is given by:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq111.gif"></p>     <p><font size="2" face="Verdana">Where: <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq148.gif"> </sub>= time step  size.</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq112.gif"></p>     <p><font size="2" face="Verdana">Once the points corresponding to parametric resonance and  those that give stable solutions are known, the regions of stability and  instability can be established, respectively.</font></p>     <p>&nbsp;</p>     ]]></body>
<body><![CDATA[<p><font size="3" face="Verdana"><b>3. 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 are developed  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.</font></p>     <p><font size="2" face="Verdana">The developing of simple closed-form expressions capable  to predict the dynamic instability regions of slender columns with semi-rigid  connections including the effects of external damping and rotary inertia under  all types of periodic axial loads is a significant advance when compared with  other complex numerical procedures that require high computing times to reach a  good enough precision.</font></p>     <p align="center"><font size="2" face="Verdana"><a name="tab02"></a></font><img src="img/revistas/dyna/v81n185/v81n185a08tab02.gif"></p>     <p align="center"><font size="2" face="Verdana"><a name="fig02"></a></font><img src="img/revistas/dyna/v81n185/v81n185a08fig02.gif"></p>     <p align="center"><font size="2" face="Verdana"><a name="fig03"></a></font><img src="img/revistas/dyna/v81n185/v81n185a08fig03.gif"></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>     ]]></body>
<body><![CDATA[<p><font size="3" face="Verdana"><b>Appendix: Derivation of instability regions</b></font></p>     <p><font size="2" face="Verdana">The equations for the borders between stable and unstable  conditions for slender columns under parametric excitation proposed herein are  based on Floquet's theory as some other researchers such as Svensson &#91;12&#93; and  Kumar and Mohammed &#91;14&#93;. A brief description of Floquet's theory is given next.</font></p>     <p><font size="2" face="Verdana">Rewriting Eq. (8b) as a system of two first-order  differential equations the following expression is obtained:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq12.gif"></p>     <p><font size="2" face="Verdana">Since <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq183.gif"></sub> is periodic, it is  clear that matrix <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq185.gif"></sub> is periodic. The  periodicity of matrix <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq185.gif"></sub> can be used to obtain  the solution of Eq. (8b) by making use of the Floquet's theory. The character  of the solutions for Eq. (8b) depends on the values of the harmonically varying  coefficients.</font></p>     <p><font size="2" face="Verdana">As shown by Timoshenko and Gere &#91;18&#93; depending on the  magnitude and frequency of the periodic axial load, stable or unstable  conditions can be reached. From Floquet's theory it is concluded that the  borders between stable and unstable conditions the solutions for Eq. (8b)  become periodic with period <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq058.gif"></sub> or <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq060.gif"></sub> with <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq186.gif"></sub>.</font></p>     <p><font size="2" face="Verdana">The solution with period <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq060.gif"></sub> is considered first  and can be expressed in the form of series expansion as follows:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq13.gif"></p>     <p><font size="2" face="Verdana">Substituting Eq. (13) into (8b) and grouping the terms  appropriately, an expression of the following form is generated:</font></p>     <p><font size="2" face="Verdana">To satisfy Eq. (18) all terms <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq191.gif"></sub> and <img src="img/revistas/dyna/v81n185/v81n185a08eq193.gif"> must be equal to zero.  Then a homogenous system of linear equations expressed in terms of <img src="img/revistas/dyna/v81n185/v81n185a08eq195.gif"> and <img src="img/revistas/dyna/v81n185/v81n185a08eq197.gif"> is produced which by  making the determinant of its matrix equal to zero then the non-trivial  solutions can be obtained as follow:</font></p>     ]]></body>
<body><![CDATA[<p><img src="img/revistas/dyna/v81n185/v81n185a08eq14151.gif"></p>     <p><font size="2" face="Verdana">The solution with period <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq060.gif"></sub> indicated by Eq. (13)  is only applicable to the odd number of regions as described by Kumar and  Mohammed &#91;14&#93;. Since closed expressions for the regions of instability are of  interest, it is necessary to consider a finite part of the determinant shown in  Eq. (19a). A sufficiently close approximation for the infinite eigenvalue  problem is obtained by taking <i>n</i>= 1  inEq. (17) according to Svensson &#91;12&#93;. Now using this approximation Eq. (15a)  is reduced to:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq152.gif"></p>     <p><font size="2" face="Verdana">Eq. (15b) gives rise to a fourth-order algebraic equation  of the form <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq206.gif"></sub> from which the  following value of <i><sub><img src="img/revistas/dyna/v81n185/v81n185a08eq208.gif"></sub> </i>can be  obtained:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq16.gif"></p>     <p><font size="2" face="Verdana">In a similar fashion the solution with period <i>T</i> can be determined taking the solution  in the form of series expansion:</font></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq17.gif"></p>     <p><font size="2" face="Verdana">Following the same procedure used for the solution with  period 2<i>T</i>, substituting Eq. (17) into  (8b) and grouping the terms appropriately, an expression of the following form  is generated:</font></p> <img src="img/revistas/dyna/v81n185/v81n185a08eq18.gif">     <p><font size="2" face="Verdana">From the solution described in Eq. (17), only the even  number of regions can be found according to Kumar and Mohammed &#91;14&#93;. As  previously stated, closed formulas for the regions of instability are of  interest, so it is necessary to consider a finite part of the determinant shown  in Eq. (19a). In a similar way, a sufficiently close approximation for the  infinite eigenvalue problem is obtained by taking<i> n</i>= 1 in  Eq. (17). By using this approximation Eq. (19b) can be obtained. Unlike the  previous case, the determinant expressed by Eq. (19b) does not produce a  fourth-order algebraic equation of the form<sub><img src="img/revistas/dyna/v81n185/v81n185a08eq216.gif"></sub>. To find an expression in this form it is necessary that  either one <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq084.gif"></sub> or <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq086.gif"></sub> be equal to zero. If  this condition is satisfied, closed expressions for the regions of instability  can be found and written as</font></p> <img src="img/revistas/dyna/v81n185/v81n185a08eq20.gif">     <p><font size="2" face="Verdana">where A, B and C are calculated as listed below.</font></p>     ]]></body>
<body><![CDATA[<p><img src="img/revistas/dyna/v81n185/v81n185a08eq201.gif"></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq202.gif"></p>     <p><img src="img/revistas/dyna/v81n185/v81n185a08eq19.gif"></p>     <p><font size="2" face="Verdana">When both <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq084.gif"></sub> and <sub><img src="img/revistas/dyna/v81n185/v81n185a08eq086.gif"></sub> are different from  zero, Eq. (20) is not applicable and the solution shall be obtained by solving  Eq. (19b).</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> C. Koning, C. and Taub, T., Impact buckling of thin bars in the elastic range hinged at both ends, Luftfahrtforschung, 10(2), pp. 55-64, 1933, (translated as NACA TM 748 in 1934).    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000119&pid=S0012-7353201400030000800001&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> Simitses, G. J. and Hodges, D. H., Fundamentals of Structural Stability, ELSEVIER Inc, Chapter 12, pp. 329-332, 2006.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000121&pid=S0012-7353201400030000800002&lng=','','width=640,height=500,resizable=yes,scrollbars=1,menubar=yes,');">Links</a>&#160;]<!-- end-ref --></font></p>     ]]></body>
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<body><![CDATA[<!-- ref --><p> <font size="2" face="Verdana"><b>&#91;8&#93;</b> Sridharan, S. and Benito, R., (1984). Columns: Static and Dynamic Interactive Buckling, J. of Engineering Mechanics, 110 (1), pp. 49-65, 1984.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000133&pid=S0012-7353201400030000800008&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;9&#93;</b> Shigematsu, T., Hara, T. and Ohga, M., Dynamic Stability Analysis by Matrix Function, J. of Engineering Mechanics, 113 (7), pp. 1085-1100, 1987.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000135&pid=S0012-7353201400030000800009&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;10&#93;</b> Sophianopoulos, D. S. and Kounadis, A. N., Dynamic Stability of Imperfect Frames Under Joint Displacements, J. of Engineering Mechanics, 120 (8), pp. 1661-1674, 1994.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000137&pid=S0012-7353201400030000800010&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;11&#93;</b> Wong, K. K. F. and Yang, R., Inelastic Dynamic Response of Structures Using Force Analogy Method,&quot; J. of Engineering Mechanics, 125 (10), pp. 1190-1199, 1999.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000139&pid=S0012-7353201400030000800011&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;12&#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=000141&pid=S0012-7353201400030000800012&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;13&#93;</b> Yabuki, T., Yasunori, A., Fumishige, A. F. and Lu, W., Nonlinear Effect on Instability of Steel Columns under Dynamic Axial Loads, J. of Structural Engineering, 131 (12), pp. 1832-1840, 2005.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000143&pid=S0012-7353201400030000800013&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;14&#93;</b> Kumar, T. H. and Mohammed, A., Finite element analysis of dynamic stability of skeletal structures under periodic loading, J. of Zhejiang University SCIENCE A, 8 (2), pp. 245-256. 2007.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000145&pid=S0012-7353201400030000800014&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;15&#93;</b> Dohnal, F., Ecker, H. and Springer, H., Enhanced damping of a cantilever beam by axial parametric excitation, Arch Appl. Mech, 78, 935&#150;947, 2008.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000147&pid=S0012-7353201400030000800015&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;16&#93;</b> Mailybaev, A. A. and Seyranian, A. P., Stabilization of statically unstable columns by axial vibration of arbitrary frequency, J. of Sound and Vibration, 328 (1-2), pp. 203&#150;212, 2009.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000149&pid=S0012-7353201400030000800016&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;17&#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: verification and examples, Revista DYNA, submitted for possible publication.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=000151&pid=S0012-7353201400030000800017&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;18&#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=000153&pid=S0012-7353201400030000800018&lng=','','width=640,height=500,resizable=yes,scrollbars=1,menubar=yes,');">Links</a>&#160;]<!-- end-ref --><p>&nbsp;</p>     <p><font size="2" face="Verdana"><b>Oliver  Giraldo-Londo&ntilde;o:</b>&nbsp;received the BS in Civil Engineering in 2010  from&nbsp;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 advice 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&nbsp;Emilio Robledo award (Colombian  Society of Engineers, 2009) and&nbsp;the Young Researcher award (COLCIENCIAS,  2010-2011). Also, he was&nbsp;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>&nbsp;received the Bachelor degree. in Civil Engineering  in 1970 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 NSF research grant in 1988. 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). 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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<surname><![CDATA[Aristizabal-Ochoa]]></surname>
<given-names><![CDATA[J. D.]]></given-names>
</name>
</person-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>
<source><![CDATA[Revista DYNA]]></source>
<year></year>
</nlm-citation>
</ref>
<ref id="B18">
<label>18</label><nlm-citation citation-type="book">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Timoshenko]]></surname>
<given-names><![CDATA[S. P]]></given-names>
</name>
<name>
<surname><![CDATA[Gere]]></surname>
<given-names><![CDATA[J. M.]]></given-names>
</name>
</person-group>
<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>
<publisher-name><![CDATA[McGraw-Hill Book Inc.]]></publisher-name>
</nlm-citation>
</ref>
</ref-list>
</back>
</article>
