<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">WJM</journal-id><journal-title-group><journal-title>World Journal of Mechanics</journal-title></journal-title-group><issn pub-type="epub">2160-049X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/wjm.2014.411034</article-id><article-id pub-id-type="publisher-id">WJM-51954</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  On a Constitutive Material Model to Capture Time Dependent Behavior of Cortical Bone
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>nders</surname><given-names>Halldin</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Mats</surname><given-names>Ander</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Magnus</surname><given-names>Jacobsson</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Stig</surname><given-names>Hansson</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib></contrib-group><aff id="aff3"><addr-line>DENTSPLY Implants, Molndal, Sweden</addr-line></aff><aff id="aff1"><addr-line>Department of Prosthodontics, Faculty of Odontology, Malmo University, Malmo, Sweden</addr-line></aff><aff id="aff2"><addr-line>Department of Applied Mechanics, Chalmers University of Technology, Goteborg, Sweden</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>anders.halldin@mah.se(NH)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>24</day><month>11</month><year>2014</year></pub-date><volume>04</volume><issue>11</issue><fpage>348</fpage><lpage>361</lpage><history><date date-type="received"><day>3</day>	<month>October</month>	<year>2014</year></date><date date-type="rev-recd"><day>2</day>	<month>November</month>	<year>2014</year>	</date><date date-type="accepted"><day>24</day>	<month>November</month>	<year>2014</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  It is commonly known that cortical bone exhibits viscoelastic-viscoplastic behavior which affects the biomechanical response when an implant is subjected to an external load. In addition, long term effects such as creep, relaxation and remodeling affect the success of the implant over time. Constitutive material models are commonly derived from data obtained in
   in vitro experiments. However during function, remodeling of bone greatly affects the bone material over time. Hence it is essential to include long term 
  in vivo effects in a constitutive model of bone. This paper proposes a constitutive material model for cortical bone incorporating viscoelasticity, viscoplasticity, creep and remodeling to predict stress-strain at various strain rates as well as the behavior of bone over time
   in vivo. The rheological model and its parameters explain the behavior of bone subjected to longitudinal loading. By a proper set of model parameters, for a specific cortical bone, the present model can be used for prediction of the behavior of this bone under specific loading conditions. In addition simulation with the proposed model demonstrates excellent agreement to 
  in vitro and 
  in vivo experimental results in the literature.
 
</p></abstract><kwd-group><kwd>Cortical bone Viscoelastic-Viscoplastic Creep Remodeling Constitutive Model</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The main function of bone is to carry load. An external load applied to bone induces strains of different magnitudes, depending on loading condition, geometry and material behavior of the bone. Numerous investigations have been conducted to examine the behavior of bone under loading [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] - [<xref ref-type="bibr" rid="scirp.51954-ref14">14</xref>] . Research has found that when cor- tical bone is loaded below yield load, the initial mechanical response is linear and can be described by Hooke’s law. Bone constitutes a hierarchical structure, where all structural levels determine the macro material properties [<xref ref-type="bibr" rid="scirp.51954-ref15">15</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref16">16</xref>] and contains of three major components, collagen, mineral and body fluid, that contribute to the me- chanical behavior. Currey [<xref ref-type="bibr" rid="scirp.51954-ref17">17</xref>] finds that Young’s modulus is correlated to the amount of hydroxyapatite, where increased content of the mineral results in higher Young’s modulus. If the load is increased, the bone reaches a yield point with an associated yield strain. Currey [<xref ref-type="bibr" rid="scirp.51954-ref17">17</xref>] further finds that bone seems to yield at a particular strain level of 0.0036 - 0.012 rather than at a particular stress level, with lower strain values for high Young’s modulus and high mineral content. Several researchers have found that bone exhibits viscoelastic properties both in tension and compression [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] - [<xref ref-type="bibr" rid="scirp.51954-ref21">21</xref>] . In these studies the material stiffness represented by Young’s modulus increased with increased strain rate but for the yield strain the results were not coherent. The results of Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] indicate that higher strain rate gives higher yield strain in tension. Similar findings were obtained by Currey [<xref ref-type="bibr" rid="scirp.51954-ref22">22</xref>] and Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] . However the results of compression test by McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] indicate that for low strain rate, the yield strain level is independent of strain rate but decreases for high strain rates. Hansen et al. [<xref ref-type="bibr" rid="scirp.51954-ref20">20</xref>] reported decreased yield strain levels for increased strain rate in tension. This contradiction in results may reflect different species, specimen sampling, specimen preparation and testing procedures. Currey [<xref ref-type="bibr" rid="scirp.51954-ref23">23</xref>] finds that the homogenized bone properties are species specific. Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] conclude that the mechanical properties and viscoelastic behavior of bone material are significantly dependent on moisture content. It has also been found that the age of the bone affects its porosity which in turn affects the mechanical properties such as ultimate stress, ultimate strain, and yield stress [<xref ref-type="bibr" rid="scirp.51954-ref24">24</xref>] . Beyond the yield strain, post yield strain occurs in the bone. Post yield strain reflects damage of the material caused by micro cracks and/or internal slip between the mineral and collagen that degrades the material until failure [<xref ref-type="bibr" rid="scirp.51954-ref13">13</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref25">25</xref>] . Studies have demonstrated that the strain rate affects the evolution of post yield strain, where lower strain rate exhibits an in- crease of post yield strain before failure [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref25">25</xref>] . Beyond yield strain, bone may withstand increased loading due to hardening before failure [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] . It has also been found that bone demonstrates relaxation over time [<xref ref-type="bibr" rid="scirp.51954-ref26">26</xref>] . According to Iyo et al. [<xref ref-type="bibr" rid="scirp.51954-ref26">26</xref>] the relaxation phenomena consists of two different processes: one fast process (relaxation time in order of 10<sup>2</sup> s) explained by relaxation of the collagen matrix and one slower relaxation (re- laxation time in order of 10<sup>6</sup> s) related to the higher order structure of the bone. Several studies have shown that bone exhibits creep phenomena including a viscoelastic creep that recovers after unloading and a creep that re- mains after unloading [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] - [<xref ref-type="bibr" rid="scirp.51954-ref30">30</xref>] . Bone is a living material and it is difficult to perform strength tests in vivo. Therefore most studies have been performed in vitro on dead bone. However a few in vivo tests exist that can be used to extract the mechanical properties of bone [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref31">31</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref32">32</xref>] . Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] installed compression plates in sheep tibia in vivo and measured the development of longitudinal forces over time. They concluded that an ini- tial decrease in axial force is related to the viscoelastic properties of bone and that a subsequent linear decrease in pressure is related to remodeling. Similar findings have been reported by Cordey et al. [<xref ref-type="bibr" rid="scirp.51954-ref32">32</xref>] and by Blumlein et al. [<xref ref-type="bibr" rid="scirp.51954-ref31">31</xref>] . Generally the remodeling rate is species dependent [<xref ref-type="bibr" rid="scirp.51954-ref33">33</xref>] . To capture the behavior of cortical bone subjected to various loading rate it is essential to have a constitutive material model that captures the stress- strain relationship for different strain rates. Johnson et al. [<xref ref-type="bibr" rid="scirp.51954-ref11">11</xref>] developed a viscoelastic-viscoplastic constitutive model that describes the stress-strain relationship for different strain rates. Their model demonstrates excellent agreement with published experimental tests results. However the Johnson et al. [<xref ref-type="bibr" rid="scirp.51954-ref11">11</xref>] model does not contain a remodeling term for biological reduction of the initiated pre-stress over time. In addition it does neither model relaxation nor creep. Furthermore, it does not reflect the hardening effect implying that the stress may increase during post yield strain. When an oversized implant is inserted into bone it induces static strains that create static stresses in the bone that gradually decline due to relaxation and remodeling. In addition, if a constant load is ap- plied strains increase in time due to creep. The objective of the present study is to develop a constitutive model for cortical bone that captures the mechanical behavior of the bone subjected to a longitudinal load. The pro- posed constitutive model with calibrated model parameters should predict the stress strain, relaxation and creep behavior observed in the in vivo and in vitro experiments.</p></sec><sec id="s2"><title>2. Theory</title><p>This work proposes a viscoelastic-viscoplastic material model with a remodeling term to describe the relationship between stress and strain in vivo. This model has similarities to that of Johnson et al. [<xref ref-type="bibr" rid="scirp.51954-ref11">11</xref>] but also captures hardening, relaxation, creep and remodeling behavior. The model is illustrated by the rheological model according to <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><p>It consists of three different components: one viscoelastic, one viscoplastic, and one remodeling component. The individual components might contain several parts, contributing to the specific behavior of bone.</p><p>The total strain according to <xref ref-type="fig" rid="fig1">Figure 1</xref> can be defined as follows:</p><disp-formula id="scirp.51954-formula1334"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x6.png"  xlink:type="simple"/></disp-formula><p>The parameters describing the material model (<xref ref-type="table" rid="table1">Table 1</xref>) are calibrated by use of experimental results, representing homogenized bone, found in the literature (<xref ref-type="table" rid="table2">Table 2</xref>).</p><p>The relationship between stress and strain for each component, respectively, is derived by the use of the dissipation inequality according to the second law of thermodynamics.</p><sec id="s2_1"><title>2.1. Viscoelastic component</title><p>During function, short term loads with different loading rates are applied which affect the bone differently due to the viscoelastic properties. To predict viscoelastic creep, relaxation and stiffness for different strain rates the proposed model consists of one spring element and four Maxwell elements in parallel (<xref ref-type="fig" rid="fig1">Figure 1</xref>).</p><p>The strain rate <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x7.png" xlink:type="simple"/></inline-formula> in the individual dashpot<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x8.png" xlink:type="simple"/></inline-formula>, of the Maxwell element, with associated viscosity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x9.png" xlink:type="simple"/></inline-formula> is defined as:</p><disp-formula id="scirp.51954-formula1335"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x10.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_2"><title>2.2. Viscoplastic component</title><p>The viscoplastic component contains a plastic pad, a dashpot and a spring in parallel. The plastic pad is activated by stresses beyond a triggering stress resulting in permanent strain. The dashpot captures the increase of stress with an increase in strain rate [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] and the spring mimics hardening of the material causing an increase in stress at post yield strain [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] . The viscoplastic component has similarities with the one in Garcia’s model [<xref ref-type="bibr" rid="scirp.51954-ref12">12</xref>] but does not include a damage criterion. However a further development, including Garcia’s [<xref ref-type="bibr" rid="scirp.51954-ref12">12</xref>] damage criterion to the spring in the viscoplastic component, may be possible. The constitutive equations for the viscoplastic- component originate from Perzyna [<xref ref-type="bibr" rid="scirp.51954-ref34">34</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref35">35</xref>] and are further described in Ottosen and Ristinmaa [<xref ref-type="bibr" rid="scirp.51954-ref36">36</xref>] .</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Illustration of the rheological model for the proposed constitutive material model of vital cortical bone in longitudinal direction. The model consists of three different components (viscoelastic, viscoplastic and remodeling) to capture stress- strain relationship, relaxation, remodeling and creep behavior</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-4900314x11.png"/></fig><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Symbols used in the modeling and definitions</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Parameter</th><th align="center" valign="middle" >Definition</th></tr></thead><tr><td align="center" valign="middle" ><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x12.png" xlink:type="simple"/></inline-formula> </sub></td><td align="center" valign="middle" >Elastic strain in spring <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x13.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x14.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Viscoelastic strain in dashpot <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x15.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x16.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Plastic strain</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x17.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Permanent creep strain</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x18.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Remodeling strain</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x19.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Elastic stiffness</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x20.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Viscosity in the elastic component</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x21.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Hardening</td></tr><tr><td align="center" valign="middle" >np</td><td align="center" valign="middle" >Plastic stress exponent</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x22.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Yield stress</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x23.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Viscosity in the plastic component</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x24.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Arbitrary reference stress</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x25.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Plastic multiplier</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x26.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >Remodeling</td></tr></tbody></table></table-wrap><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Overview of experimental studies referred to in the present study</title></caption><table><tbody><thead><tr><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle"  colspan="4"  >Aspects of the mechanical behavior of bone</th><th align="center" valign="middle"  colspan="2"  ></th></tr></thead><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >Stress strain</td><td align="center" valign="middle" >Creep</td><td align="center" valign="middle" >Relaxation</td><td align="center" valign="middle" >Remodeling</td><td align="center" valign="middle"  colspan="2"  >Comment</td></tr><tr><td align="center" valign="middle"  rowspan="5"  >Experiment</td><td align="center" valign="middle" >Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>]</td><td align="center" valign="middle" >Tension</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >In vitro</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" >McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>]</td><td align="center" valign="middle" >Compression</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >In vitro</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" >Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>]</td><td align="center" valign="middle" >Tension</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >In vitro</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" >Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>]</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >Tension</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >In vitro</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" >Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>]</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >Compression</td><td align="center" valign="middle" >Compression</td><td align="center" valign="middle" >In vivo</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" >Present model</td><td align="center" valign="middle" >Parameters that were calibrated to capture the mechanical behavior found in experiments</td><td align="center" valign="middle" >E<sub>1</sub>-E<sub>5</sub> u<sub>4</sub> and u<sub>5</sub> s<sub>y</sub>, H and u<sub>p</sub></td><td align="center" valign="middle" >E<sub>3</sub> and u<sub>3</sub></td><td align="center" valign="middle" >E<sub>2</sub> and u<sub>2</sub></td><td align="center" valign="middle" >u<sub>r</sub></td><td align="center" valign="middle" >Simulation</td><td align="center" valign="middle" ></td></tr></tbody></table></table-wrap><p>The yield function<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x27.png" xlink:type="simple"/></inline-formula>, according to Ottosen and Ristinmaa [<xref ref-type="bibr" rid="scirp.51954-ref36">36</xref>] , is defined as</p><disp-formula id="scirp.51954-formula1336"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x28.png"  xlink:type="simple"/></disp-formula><p>where the yield evolves when<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x29.png" xlink:type="simple"/></inline-formula>.</p><p>The plastic strain rate is defined as</p><disp-formula id="scirp.51954-formula1337"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x30.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.51954-formula1338"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x31.png"  xlink:type="simple"/></disp-formula><p>An overstress function <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x32.png" xlink:type="simple"/></inline-formula> is defined according to the Norton creep power law [<xref ref-type="bibr" rid="scirp.51954-ref37">37</xref>] :</p><disp-formula id="scirp.51954-formula1339"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x33.png"  xlink:type="simple"/></disp-formula><p>The stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x34.png" xlink:type="simple"/></inline-formula> is an arbitrary reference stress. It is postulated that:<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x35.png" xlink:type="simple"/></inline-formula>.</p></sec><sec id="s2_3"><title>2.3. Remodeling component</title><p>The linear decrease in force in Perren’s et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] in vivo experiment is interpreted as a reduction in stress due to remodeling of bone. In the present study the reduction of stress is modeled as a constant reduction of strain over time and the remodeling component is therefore expressed in terms of a constant strain rate:</p><disp-formula id="scirp.51954-formula1340"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x36.png"  xlink:type="simple"/></disp-formula><p>In the proposed model we define a remodeling parameter <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x37.png" xlink:type="simple"/></inline-formula> to:</p><disp-formula id="scirp.51954-formula1341"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x38.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_4"><title>2.4. Differential equation for the proposed bone model</title><p>By adding the different components into the rheological model, the differential equation for each spring-dash- pot-combination is derived.</p><p>Spring 1</p><disp-formula id="scirp.51954-formula1342"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x39.png"  xlink:type="simple"/></disp-formula><p>Spring 2- 4</p><disp-formula id="scirp.51954-formula1343"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-4900314x40.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_5"><title>2.5. Calibration of model parameters</title><p>The magnitude of the viscoelastic, viscoplastic, relaxation, creep and remodeling parameters were obtained by fitting the model simulations to experimental results [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] by minimizing the error. The minimized error was found by using the constrained nonlinear optimization function (FMINSEARCHCON) available in MATLAB.</p></sec><sec id="s2_6"><title>2.6. Viscoelastic and viscoplastic stress-strain behavior</title><p>The viscoelastic and viscoplasticstress-strain behavior of cortical bone is reported in Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] , McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] and Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] . The simulations, by use of the proposed constitutive model with the calibrated parameter values, mimic the stress strain curves in these in vitro experimental studies.</p></sec><sec id="s2_7"><title>2.7. Relaxation and remodeling behavior</title><p>The relaxation and remodeling behavior of cortical bone was identified using three in vivo data sets of reduction in force with time obtained from Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] . The proposed model presents relaxation as a reduction of stress with time. Therefore the axial force was converted to stress by assuming a cross sectional area of 160 mm<sup>2</sup> for one sheep tibia. The other two sheep tibiae cross sectional areas were thereafter set to 186 and 290 mm<sup>2</sup> respectively resulting in the same remodeling rate for the different sheep. The measurements in Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] started 3 h after the initiation of bone compression. Therefore the initial (at 0 s) strain level was adjusted to fit the measurements at 3 h in Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] .</p></sec><sec id="s2_8"><title>2.8. Reversible and irreversible creep behavior</title><p>Creep behavior was identified using creep curves from the experiments of Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] . Four different magnitudes of constant stress for the individual stress-strain tests were used (20%, 30%, 40% and 50% of ultimate stress<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x41.png" xlink:type="simple"/></inline-formula>). The ultimate stress (in Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x42.png" xlink:type="simple"/></inline-formula>= 112 MPa, in McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x43.png" xlink:type="simple"/></inline-formula>= 144 MPa and Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x44.png" xlink:type="simple"/></inline-formula>= 141 MPa) was determined by use of stress-strain curves at strain rates of 0.001 s<sup>−1</sup> respectively. The constant stress was applied during 12,000 s and then released. For simulation purposes the stress was ramped up to a constant level during 1 s and ramped down during 1 s.</p></sec></sec><sec id="s3"><title>3. Results</title><p>Applying appropriate parameters values the predictions of the mechanical behavior of the bone agrees well with the results in experimental tests according to Figures 2-5.</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Stress-strain curves predicted by the proposed model with corresponding experimental data for (a) Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] (b) McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] and (c) Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] </title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-4900314x45.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Prediction of creep behavior by the proposed model for the stress-strain tests of (a) Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] (b) Mc Elhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] and (c) Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] with corres- ponding experimental data from Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] </title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-4900314x46.png"/></fig><p>The parameters for the viscoelastic component are presented in <xref ref-type="table" rid="table3">Table 3</xref>.</p><p>It seems that individual spring stiffness E<sub>1</sub>, E<sub>2</sub>, E<sub>3</sub>, E<sub>4</sub>, and E<sub>5</sub>, are 25% - 28%, 11% - 12%, 3% - 5%, 9% - 10% and 48% - 50%, respectively of total Young’s modulus (sum (E<sub>1</sub> to E<sub>5</sub>)) regardless of stress strain test (<xref ref-type="table" rid="table4">Table 4</xref>).</p><p>The values obtained for the viscosity parameter u<sub>2</sub> are in the same range when fitting the model to the experimental results of Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] , McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] and Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] , representing relaxation times t<sub>2</sub> of 3.3, 3.9 and 4.1 days respectively (<xref ref-type="table" rid="table3">Table 3</xref>). The viscosity parameter u<sub>3 </sub>represents fast relaxation with relaxation times t<sub>3 </sub>in the range of 1200 - 1330 s (<xref ref-type="table" rid="table3">Table 3</xref>). The viscosity parameters u<sub>4</sub> and u<sub>5 </sub>represent even faster relaxation with relaxation times t<sub>4</sub> and t<sub>5</sub> in the range of 100 - 400 ms and 1 - 20 &#181;s respectively</p><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Prediction of reverse creep behavior by the proposed model for the stress-strain tests of (a) Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] (b) Mc Elhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] and (c) Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] with corres- ponding experimental data from Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] </title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-4900314x47.png"/></fig><p>(<xref ref-type="table" rid="table3">Table 3</xref>). The values of the individual parameters obtained for the viscoplastic component, when fitting the model to the experimental results of Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] , McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] and Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] , clearly differ (<xref ref-type="table" rid="table5">Table 5</xref>).</p><p>To capture the stress strain behavior for all strain rate experiments <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x48.png" xlink:type="simple"/></inline-formula> must be in the range of the yield point for the stress strain curve for the lowest strain rate. In the present model the value of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x48.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x49.png" xlink:type="simple"/></inline-formula> shall be seen as a triggering value for the viscoplastic behavior for all strain rates. However to significantly evolve plastic strain</p><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Prediction of relaxation and remodeling behavior by the proposed model for the stress-strain tests of (a) Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] (b) McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] and (c) Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] with corresponding experimental data from Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] </title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-4900314x50.png"/></fig><p>(representing material yield) for increased strain rate increased stress is required. The stress-strain test (<xref ref-type="fig" rid="fig2">Figure 2</xref>(a)) of Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] resulted in a higher value of the hardening coefficient <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x51.png" xlink:type="simple"/></inline-formula> compared to the other stress-strain tests (<xref ref-type="fig" rid="fig2">Figure 2</xref>(b), <xref ref-type="fig" rid="fig2">Figure 2</xref>(c)) [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] . In addition the magnitude of the yield stress value is higher for McElhaney’s [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] compressive test compared to those of the tensile tests [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] . The parameter value obtained for the remodeling <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x51.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x52.png" xlink:type="simple"/></inline-formula> component is presented in <xref ref-type="table" rid="table6">Table 6</xref>.</p><table-wrap id="table3" ><label><xref ref-type="table" rid="table3">Table 3</xref></label><caption><title> Parameters, for the individual stress-strain tests, of the viscoelastic component according to <xref ref-type="fig" rid="fig1">Figure 1</xref> with time constants t. The parameters are calibrated by means of the least square method to fit stress-strain, relaxation, remodeling and creep experimental data.</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="2"  >Model parameter</th><th align="center" valign="middle"  colspan="3"  >The magnitude of the viscoelastic parameters</th></tr></thead><tr><td align="center" valign="middle" >Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>]</td><td align="center" valign="middle" >McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>]</td><td align="center" valign="middle" >Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>]</td></tr><tr><td align="center" valign="middle" >E<sub>1</sub> [Mpa]</td><td align="center" valign="middle" >8989</td><td align="center" valign="middle" >10,175</td><td align="center" valign="middle" >6904</td></tr><tr><td align="center" valign="middle" >E<sub>2 </sub>[Mpa]<sub> </sub></td><td align="center" valign="middle" >4167</td><td align="center" valign="middle" >4355</td><td align="center" valign="middle" >2828</td></tr><tr><td align="center" valign="middle" >E<sub>3 </sub>[Mpa]<sub> </sub></td><td align="center" valign="middle" >1797</td><td align="center" valign="middle" >1678</td><td align="center" valign="middle" >739</td></tr><tr><td align="center" valign="middle" >E<sub>4 </sub>[Mpa]<sub> </sub></td><td align="center" valign="middle" >3587</td><td align="center" valign="middle" >4221</td><td align="center" valign="middle" >2065</td></tr><tr><td align="center" valign="middle" >E<sub>5 </sub>[Mpa]<sub> </sub></td><td align="center" valign="middle" >17,890</td><td align="center" valign="middle" >20,729</td><td align="center" valign="middle" >11,699</td></tr><tr><td align="center" valign="middle" >u<sub>2 </sub>[Mpa s]</td><td align="center" valign="middle" >1.2E+09</td><td align="center" valign="middle" >1.5E+09</td><td align="center" valign="middle" >9.9E+08</td></tr><tr><td align="center" valign="middle" >u<sub>3 </sub>[Mpa s]</td><td align="center" valign="middle" >2.2E+06</td><td align="center" valign="middle" >2.2E+06</td><td align="center" valign="middle" >9.8E+05</td></tr><tr><td align="center" valign="middle" >u<sub>4 </sub>[Mpa s]</td><td align="center" valign="middle" >5.1E+02</td><td align="center" valign="middle" >8.3E+02</td><td align="center" valign="middle" >6.9E+02</td></tr><tr><td align="center" valign="middle" >u<sub>5 </sub>[Mpa s]</td><td align="center" valign="middle" >3.8E−01</td><td align="center" valign="middle" >2.6E−01</td><td align="center" valign="middle" >1.6E−02</td></tr><tr><td align="center" valign="middle" >t<sub>2</sub> [s (days)]</td><td align="center" valign="middle" >2.9E+05 (3.3)</td><td align="center" valign="middle" >3.4E+05 (3.9)</td><td align="center" valign="middle" >3.5E+05 (4.1)</td></tr><tr><td align="center" valign="middle" >t<sub>3</sub>[s]</td><td align="center" valign="middle" >1203</td><td align="center" valign="middle" >1313</td><td align="center" valign="middle" >1330</td></tr><tr><td align="center" valign="middle" >t<sub>4</sub> [ms]</td><td align="center" valign="middle" >141</td><td align="center" valign="middle" >197</td><td align="center" valign="middle" >334</td></tr><tr><td align="center" valign="middle" >t<sub>5</sub>[&#181;s]</td><td align="center" valign="middle" >21</td><td align="center" valign="middle" >13</td><td align="center" valign="middle" >1.4</td></tr></tbody></table></table-wrap><table-wrap id="table4" ><label><xref ref-type="table" rid="table4">Table 4</xref></label><caption><title> Contributions in % to the total Young’s modulus of the springs in the viscoelastic component, for the individual stress-strain tests, indicating the same distribution independent of test</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Ratio</th><th align="center" valign="middle" >Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>]</th><th align="center" valign="middle" >McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>]</th><th align="center" valign="middle" >Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>]</th></tr></thead><tr><td align="center" valign="middle" ><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x53.png" xlink:type="simple"/></inline-formula> </sub></td><td align="center" valign="middle" >25%</td><td align="center" valign="middle" >25%</td><td align="center" valign="middle" >28%</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x54.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >11%</td><td align="center" valign="middle" >11%</td><td align="center" valign="middle" >12%</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x55.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >5%</td><td align="center" valign="middle" >4%</td><td align="center" valign="middle" >3%</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x56.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >10%</td><td align="center" valign="middle" >10%</td><td align="center" valign="middle" >9%</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-4900314x57.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >49%</td><td align="center" valign="middle" >50%</td><td align="center" valign="middle" >48%</td></tr></tbody></table></table-wrap><table-wrap id="table5" ><label><xref ref-type="table" rid="table5">Table 5</xref></label><caption><title> Parameters for the stress-strain tests of the viscoplastic component according to <xref ref-type="fig" rid="fig1">Figure 1</xref></title></caption><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="2"  >Parameter</th><th align="center" valign="middle"  colspan="3"  >Magnitude of the plasticity parameters</th></tr></thead><tr><td align="center" valign="middle" >Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>]</td><td align="center" valign="middle" >McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>]</td><td align="center" valign="middle" >Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>]</td></tr><tr><td align="center" valign="middle" >H [Mpa]</td><td align="center" valign="middle" >297</td><td align="center" valign="middle" >75</td><td align="center" valign="middle" >114</td></tr><tr><td align="center" valign="middle" >np</td><td align="center" valign="middle" >9.5</td><td align="center" valign="middle" >12.1</td><td align="center" valign="middle" >13.5</td></tr><tr><td align="center" valign="middle" >s<sub>y</sub> [Mpa]</td><td align="center" valign="middle" >38.1</td><td align="center" valign="middle" >60.5</td><td align="center" valign="middle" >46.6</td></tr><tr><td align="center" valign="middle" >u<sub> p</sub><sub> </sub>[Mpa s]</td><td align="center" valign="middle" >9.2E+08</td><td align="center" valign="middle" >1.7E+09</td><td align="center" valign="middle" >3.0E+10</td></tr></tbody></table></table-wrap><table-wrap id="table6" ><label><xref ref-type="table" rid="table6">Table 6</xref></label><caption><title> Parameters for the stress-strain tests of the remodeling component according to <xref ref-type="fig" rid="fig1">Figure 1</xref></title></caption><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="2"  >Parameter</th><th align="center" valign="middle"  colspan="3"  >Magnitude of the remodeling parameter</th></tr></thead><tr><td align="center" valign="middle" >Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>]</td><td align="center" valign="middle" >McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>]</td><td align="center" valign="middle" >Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>]</td></tr><tr><td align="center" valign="middle" >R [s<sup>−1</sup>]</td><td align="center" valign="middle" >2.4E−11</td><td align="center" valign="middle" >2.1E−11</td><td align="center" valign="middle" >3.1E−11</td></tr></tbody></table></table-wrap></sec><sec id="s4"><title>4. Discussion</title><p>Based on the results of the present study it can be concluded that the proposed model, with a suitable choice of model parameters reflecting the properties of the bone, is capable to predict the mechanical behavior of the bone. Simulations of the mechanical response, with the proposed model and calibrated model parameters, capture with good agreement the experimental stress-strain results obtained by Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] , McElhaney [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] , Crowninshield and Pope [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] , Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] and Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] (Figures 3-5). Bone behaves differently in tension and compression [<xref ref-type="bibr" rid="scirp.51954-ref38">38</xref>] . Both tension and compression can be simulated by the present model. To capture compressive or tensile behavior the model parameters have to be determined by use of compressive or tensile test respectively. In addition the proposed model, with calibrated parameters, seems to be able to capture the creep and relaxation behavior. Bone is a complex material and the diversity of the measured bone material properties might reflect the quality, porosity, and testing condition of the bone specimen. In the proposed model the individual phenomena (viscoelasticity, plasticity, relaxation, creep and remodeling) are represented with three components reflecting the behavior of bone. The viscoelastic component contains four Maxwell elements (spring- dashpot combinations) that capture the strain rate dependency in the stress strain tests and the viscoelastic behavior found in relaxation and creep tests. The dashpots in Maxwell elements two and three have low viscosity and do not significantly influence the stress-strain curve. The increased Young’s modulus with increased strain rate is modeled, with Maxwell elements four and five. The sums of spring stiffness one to three for the individual tests [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] are similar to the Young’s modulus presented by Johnson et al. [<xref ref-type="bibr" rid="scirp.51954-ref11">11</xref>] . In the proposed model the plasticity component, with Norton creep, predicts the evolution of plastic strain at different yield stress levels for different strain rates observed in experiments (<xref ref-type="fig" rid="fig2">Figure 2</xref>). In the prediction of stress strain behavior the plastic pad in the proposed model has one triggering stress independent of strain rate. The triggering stress is lower than the physical yield stress observed in experiments in order to capture the stress-strain at low strain rates. This might reflect the observation that bone exhibits small irreversible strain, at quite low stress levels, due to sliding between the mineral and collagen as described by Mercer et al. [<xref ref-type="bibr" rid="scirp.51954-ref13">13</xref>] .</p><p>Iyo et al. [<xref ref-type="bibr" rid="scirp.51954-ref3">3</xref>] found that bone exhibits a slow relaxation in the order of 10<sup>6</sup><sup> </sup>- 10<sup>7</sup> s and a fast relaxation in the order of 10<sup>2</sup> s. In the present model the slow relaxation is governed by the Maxwell element number two in the viscoelastic component (<xref ref-type="fig" rid="fig1">Figure 1</xref>) and the parameter values were derived from the in vivo experiment by Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] , resulting in a shorter relaxation time than that found by Iyo et al. [<xref ref-type="bibr" rid="scirp.51954-ref3">3</xref>] . The parameter values obtained from the data of Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] originate from in vivo tests and bone properties in live animals is probably different from those of Iyo et al. [<xref ref-type="bibr" rid="scirp.51954-ref3">3</xref>] investigating bone samples in vitro. Many factors, such as species, specimen type, storing and testing conditions, affect the material properties of bone [<xref ref-type="bibr" rid="scirp.51954-ref17">17</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref24">24</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref39">39</xref>] . The initial drop in compression force within 14 days found by Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] can be explained by slow relaxation phenomena since the first registration of Perren&#180;s et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] was recorded 3 h after the initiated loading excluding the fast relaxation. The slow relaxation has been explained by Iyo et al. [<xref ref-type="bibr" rid="scirp.51954-ref26">26</xref>] to be related to the structural anisotropy of bone. In the studies by Halldin et al. [<xref ref-type="bibr" rid="scirp.51954-ref40">40</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref41">41</xref>] , where an oversized implant was inserted in rabbit tibiae, a decrease in removal torque with longer implantation times was found. This decrease can be explained by the slow relaxation of bone. In the proposed model the parameter values in Maxwell element number three in the viscoelastic component (<xref ref-type="fig" rid="fig1">Figure 1</xref>) were obtained from the creep experiment of Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] . The dashpot in Maxwell element three has a relaxation time of 1200 - 1300 s and differs one order of magnitude from those obtained by Iyo et al. [<xref ref-type="bibr" rid="scirp.51954-ref26">26</xref>] . The fast relaxation has been suggested by Iyo et al. [<xref ref-type="bibr" rid="scirp.51954-ref26">26</xref>] to be caused by relaxation of the collagen. Maxwell elements four and five have even shorter relaxation times of 1.4 - 3.3 ms and 1.4 - 21 &#181;s respectively and model the Young’s modulus dependence of strain rate. The decrease in force after 14 days found by Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] and Blumlein et al. [<xref ref-type="bibr" rid="scirp.51954-ref31">31</xref>] was explained as a consequence of bone remodeling and seems to be linear over time. Therefore, in the suggested model, the remodeling component is expressed in terms of a constant strain rate reducing the stress over time. The proposed model, with calibrated parameter values, predicts with good agreement the slow relaxation and remodeling phenomena published by Perren et al. [<xref ref-type="bibr" rid="scirp.51954-ref8">8</xref>] (<xref ref-type="fig" rid="fig5">Figure 5</xref>). The total creep strain consists of two parts, one viscoelastic part that recovers when load is removed and one non-reversible viscoplastic part (<xref ref-type="fig" rid="fig1">Figure 1</xref>). The creep and reverse creep behavior of the proposed model, with calibrated parameters from the three different stress-strain tests [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] , are similar to those of the creep tests performed by Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] (<xref ref-type="fig" rid="fig3">Figure 3</xref>, <xref ref-type="fig" rid="fig4">Figure 4</xref>). In a constant load situation the low viscosity of the dashpots four and five makes the viscous strain occur instantly. Thus they do not contribute to creep or reversed creep strains. The high viscosity of dashpot two, with a relaxation time in the range of 3.3 - 4.1 days, does not contribute significantly to the creep strain within the test time of 3.3 h (12,000 s) applied by Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] . Thus the viscoelastic creep observed in Melnis et al. [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] is mainly captured by Maxwell element three as earlier discussed. The permanent deformation of bone has been suggested as a consequence of sliding between collagen and mineral that does not recover during unloading [<xref ref-type="bibr" rid="scirp.51954-ref13">13</xref>] . Non-recoverable creep strain in the viscoplastic component occurs when the yield condition is satisfied according to Equation (3). In the experiments of Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] non-recoverable creep strains occurred at stress levels below 40% of the ultimate stress, which is below the triggering stress of the plastic pad in the present study (<xref ref-type="table" rid="table5">Table 5</xref>). Therefore the present model is not able to capture the low non-recoverable creep strain behavior at low stress found by Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] . Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref27">27</xref>] indicated that a stress level around 50% of the ultimate stress may result in constant strain rate (secondary creep). In the simulations with the present model a constant strain rate was only obtained with parameter values derived from the stress-strain tests of Melnis and Knets [<xref ref-type="bibr" rid="scirp.51954-ref18">18</xref>] and a constant load corresponding to 50% of ultimate strength (<xref ref-type="fig" rid="fig3">Figure 3</xref>(a)). This secondary creep originates from an increase in strain of the viscoplastic component, which was not obtained for the other simulations. However with an increased stress level, simulations of the other tests [<xref ref-type="bibr" rid="scirp.51954-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.51954-ref4">4</xref>] (<xref ref-type="fig" rid="fig3">Figure 3</xref>(b), <xref ref-type="fig" rid="fig3">Figure 3</xref>(c)) would have exhibited similar creep behavior as <xref ref-type="fig" rid="fig3">Figure 3</xref>(a).</p></sec><sec id="s5"><title>5. Conclusions</title><p>Analyzing the mechanical behavior of cortical bone during different longitudinal loading situations i.e. in vitro stress-strain relationship, in vivo relaxation, in vitro creep and in vivo remodeling has led to a proposed constitutive material model with associated rheological model that consists of four different components:.</p><p>1) A viscoelastic component modeling: a) the strain rate effect on Young’s modulus; b) the viscoelastic creep and c) the fast and slow relaxation. The viscoelastic component comprises 5 parts that can be tuned individually to achieve a desired model behavior.</p><p>2) A viscoplastic component triggering a) evolution of plastic strain and b) material hardening developed at different strain rates. In addition the viscoplastic component captures the secondary creep behavior.</p><p>3) A remodeling component modeling the decrease in prestress found in in vivo experiments. The decrease in prestress is interpreted as an effect of bone remodeling.</p><p>Depending on the simulation purpose the individual parts and/or components of the model may be included or excluded. The values of associated parameters should be determined by use of relevant experimental tests of bone.</p></sec><sec id="s6"><title>Acknowledgements</title><p>This work was supported by the Swedish Research Council (621-2010-4760).</p></sec><sec id="s7"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.51954-ref1"><label>1</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>McElhaney</surname><given-names> J.H. </given-names></name>,<etal>et al</etal>. 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