<?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.2015.512026</article-id><article-id pub-id-type="publisher-id">WJM-62117</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>
 
 
  Analytical Model on Steel Tanks Damaged by Corrosion
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>rancisco</surname><given-names>Casanova-del-Angel</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>Moisés</surname><given-names>Gaytán-López</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>SACM SMA, Government of Mexico City, Mexico City, Mexico</addr-line></aff><aff id="aff1"><addr-line>National Polytechnic Institute, Mexico City, Mexico</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>fcasanova@ipn.mx(RC)</email>;<email>mogalo_750315@hotmail.com(MG)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>10</day><month>12</month><year>2015</year></pub-date><volume>05</volume><issue>12</issue><fpage>274</fpage><lpage>285</lpage><history><date date-type="received"><day>22</day>	<month>October</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>19</month>	<year>December</year>	</date><date date-type="accepted"><day>22</day>	<month>December</month>	<year>2015</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>
 
 
  The mechanical behavior of steel employed in the hull of a steel tank damaged by corrosion has been analyzed. The tank was used to filter a deep-water well for an 8-year period. Influence of porosity and dissolution of material may be introduced in the main constitutive relation adding a new damage variable C, which describes electrochemical damage. An elastoplastic theoretical model coupled to damage of a member, and other for damage related to thermodynamic energy are developed. This theoretical development has been used to analyze mechanical behavior of steel used in the body of a steel tank damaged by corrosion in water purifier plants, Eastern System, Mexico City, where three of every ten filters show excessive corrosion inside the steel plate filtration tanks. With samples taken from steel of the tank’s hull and reinforcement of false bottom supporting filtering material inside the tank, metallography tests were carried out; localized and generalized types of corrosion were determined, as well as the type of corrosion composites generated due to anticorrosive coating used inside the tank from its manufacturing.
 
</p></abstract><kwd-group><kwd>Structural Corrosion</kwd><kwd> Damage Mechanics</kwd><kwd> Steel</kwd><kwd> Spectrometry</kwd><kwd> Tensile Stress Loss</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>In presence of high magnitude overloads, structures show damage symptoms, characterized by degradation of elastoplastic properties. This is called damaging process. The structure, as in an uniaxial assay, goes through an elastic phase modeled by elastic behavior laws and, then, through a plastic phase with hardening (modeled by the elastoplastic behavior with hardening laws). Such hardening process is gradually lowered due to the damaging process, until the last load of the structure is reached and beginning a softening process, where damage rules over hardening, finally breaking the probe, even causing solicitation of an imposed displacement. The state law, considering the damage, is obtained taking into consideration the damaged area, as we will see throughout our theoretical development, entitled: Development of a model for damage related to thermodynamic energy.</p><p>Related to control of incrustation and corrosion when water is in rain form, it may be supposed that it is chemically balanced with the surrounding environment. When touching the soil, water dissolves certain mineral components of such, among others, calcium and bicarbonate ions. Carbon dioxide required for the reaction is continually obtained from decomposition and oxidation of organic matter of the soil due to activity of microorganisms. When water rich in calcium ions and bicarbonate is extracted from the soil and is re-exposed to air, reaction becomes inverted, carbon dioxide escapes to the air and calcium carbonate also precipitates once more.</p><p>Constitutive models define a relation between stresses and strains. Constitutive models comprised in mechanics of continuous media are presented as a promising tool to treat structural response, allowing calculation of geometrically complex structures based on finite elements codes, which allow putting together various constitutive phenomena into one formulation.</p></sec><sec id="s2"><title>2. Mechanical Damage</title><p>The <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x6.png" xlink:type="simple"/></inline-formula> scalar damage variable is defined as the ratio of the damaged area A<sub>d</sub> to the nominal area A may be expressed as follows:</p><disp-formula id="scirp.62117-formula763"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x7.png"  xlink:type="simple"/></disp-formula><p>where D<sub>n</sub> is the damage variable towards n direction, A is the intersection area with the plane, and A<sub>d</sub> is the effective area damaged by corrosion, contained in A.</p><p>The value of D scalar damage variable is between 0 and 1 (0 ≤ D ≤ 1). D = 0, for a material without damage, and D = 1 for a material completely broken. In fact, failure occurs in a D &lt; 1 value, through instability process.</p><p>The term effective stress, related to the effective surface resisting load, (A - A<sub>d</sub>), is:</p><disp-formula id="scirp.62117-formula764"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x8.png"  xlink:type="simple"/></disp-formula><p>Introducing in (2) the damage variable</p><disp-formula id="scirp.62117-formula765"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x9.png"  xlink:type="simple"/></disp-formula><p>Thus obtaining Equation (4):</p><disp-formula id="scirp.62117-formula766"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x10.png"  xlink:type="simple"/></disp-formula><p>Equation (4) defines effective stress in a material under tension. Finally, strain equivalent to the principle proposed by Lemaitre used in the elastic damage scalar classical form is:</p><disp-formula id="scirp.62117-formula767"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x11.png"  xlink:type="simple"/></disp-formula><p>In this model, the mechanical effect of progressive surface loss caused by corrosion and external load is described by a single internal variable, which degrades Young’s model for material. The constitutive relation is:</p><disp-formula id="scirp.62117-formula768"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x12.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x13.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x14.png" xlink:type="simple"/></inline-formula> are the components of stress tensor and strain, respectively (i, j, k &amp; l &#206; [1, 3]), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x15.png" xlink:type="simple"/></inline-formula>is the starting rigidity module, and D is the damage variable defined before. Material is isotropic at the beginning and, together with E and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x16.png" xlink:type="simple"/></inline-formula>, Young’s model and Poisson relation are respectively considered.</p></sec><sec id="s3"><title>3. Damage by Corrosion</title><p>Since increase in material dissolution, in turn, increases porosity, its mechanical influence has been considered to be similar to the increase of holes and micro fissures, thus producing degradation of material in the area being damaged. In light of this, it is logical to introduce variable C in the stress-strain relation, in a similar way to the treatment of mechanical damage C, also within 1 and 0: where 0 for a material without electrochemical damage and 1 for a material completely dissolved. The stress-strain relation containing the two types of damage, both mechanical and corrosion, is given in (7):</p><disp-formula id="scirp.62117-formula769"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x17.png"  xlink:type="simple"/></disp-formula><p>where C is the variable for damage by corrosion obtained through an electrochemical measure system, calibrated to obtain a behavior similar to mechanical damage D. It should be noticed that a similar approach was obtained for chemical damage in [<xref ref-type="bibr" rid="scirp.62117-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.62117-ref2">2</xref>] .</p><p>For calculation of damage parameter D, the damaged area value is obtained through (8), <xref ref-type="fig" rid="fig1">Figure 1</xref>, where A is the nominal area, w and t are the dimensions of the damaged area, D<sub>n</sub> is the scalar damage variable, A<sub>d</sub> is the damaged area and a is the thickness with corrosion damage.</p><disp-formula id="scirp.62117-formula770"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x18.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62117-formula771"><graphic  xlink:href="http://html.scirp.org/file/5-4900380x19.png"  xlink:type="simple"/></disp-formula><sec id="s3_1"><title>3.1. Elastoplastic Model Coupled to Damage of a Member</title><p>Generalized strains in joints in an elastic joints with damage and plasticity are expressed through equation (9) and are:</p><disp-formula id="scirp.62117-formula772"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x20.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x21.png" xlink:type="simple"/></inline-formula> is the strain of elastic beam, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x22.png" xlink:type="simple"/></inline-formula>is the plastic strain, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x23.png" xlink:type="simple"/></inline-formula>is the strain due to damage, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x24.png" xlink:type="simple"/></inline-formula>is the flexibility matrix of an elastic beam column in starting state without damage and {M} the matrix of the main directions of damage.</p><p>Supposing there is an axial generalized stress N without buckling, the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x25.png" xlink:type="simple"/></inline-formula> relation allows obtaining a generalized stress-strain relation. With a uniform damage condition, the following is obtained:</p><disp-formula id="scirp.62117-formula773"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x26.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x27.png" xlink:type="simple"/></inline-formula></p><p>On the other hand, in accordance with the concentrated elasticity model, generalized strains of the member are expressed through the following relation:</p><disp-formula id="scirp.62117-formula774"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x28.png"  xlink:type="simple"/></disp-formula><p>Deleting the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x29.png" xlink:type="simple"/></inline-formula> term between Equations (10) and (11) we obtain:</p><disp-formula id="scirp.62117-formula775"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x30.png"  xlink:type="simple"/></disp-formula><p>Equation (12) means that, in order to obtain a concentrated an elasticity model equivalent to that obtained through damage of continuous media theory, it is necessary to define axial generalized strain. It may be ob-</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Mechanical damage</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x31.png"/></fig><p>served that, when damage has a zero value and joints have null flexibility (or an infinite rigidity), they behave as rigid-plastic connecting rods. If damage is equal to one, flexibility is infinite. In this case, it is equivalent to imagine that joints and beam column are disconnected and, therefore, the system may not transmit axial load.</p><p>Theoretical developments tells us that, when there are buckling effects, behavior is too complex to obtain explicit analytic expressions similar to Equation (12) valid for the general case, even using extremely simple damage evolution laws. Therefore, the existence of a set of damage internal variables <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x32.png" xlink:type="simple"/></inline-formula> is presented which may, as the damage of continuous media variable, have values within the [0, 1] interval, such that behavior of an elastic joints may be expressed as:</p><disp-formula id="scirp.62117-formula776"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x33.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x34.png" xlink:type="simple"/></inline-formula> is a diagonal matrix which non-null terms are the elements of its diagonal:</p><disp-formula id="scirp.62117-formula777"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x35.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x36.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x37.png" xlink:type="simple"/></inline-formula> parameters represent a measurement of buckling damage in joints i and j, respectively. Therefore, the state law of a degradable elastoplastic member is obtained substituting equation (14) in Equation (13):</p><disp-formula id="scirp.62117-formula778"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x38.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x39.png" xlink:type="simple"/></inline-formula> is the flexibility matrix of a degradable member and in the specific case of small strains:</p><disp-formula id="scirp.62117-formula779"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x40.png"  xlink:type="simple"/></disp-formula><p>With <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x41.png" xlink:type="simple"/></inline-formula> the rigidity matrix of a degradable member. And for the specific case of a constant transversal section member with area A, inertia I, elasticity module E and length l, the rigidity matrix elements <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x42.png" xlink:type="simple"/></inline-formula> are expressed as follows:</p><disp-formula id="scirp.62117-formula780"><graphic  xlink:href="http://html.scirp.org/file/5-4900380x43.png"  xlink:type="simple"/></disp-formula><p>As it may be verified, in case of the existence of a completely degraded joint <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x44.png" xlink:type="simple"/></inline-formula> the degraded rigidity matrix coincides with that of a member with an internal joint. And the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x45.png" xlink:type="simple"/></inline-formula> damage variable reduces rigidity of the member in presence of axial actions.</p><p>Complementary strain energy of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x46.png" xlink:type="simple"/></inline-formula> member may be expressed as the addition of the complementary strain energy of the elastic beam column <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x46.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x47.png" xlink:type="simple"/></inline-formula> and the complementary strain energy of joints:</p><disp-formula id="scirp.62117-formula781"><graphic  xlink:href="http://html.scirp.org/file/5-4900380x48.png"  xlink:type="simple"/></disp-formula><p>And small strains</p><disp-formula id="scirp.62117-formula782"><graphic  xlink:href="http://html.scirp.org/file/5-4900380x49.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62117-formula783"><graphic  xlink:href="http://html.scirp.org/file/5-4900380x50.png"  xlink:type="simple"/></disp-formula><p>where U is the strain energy.</p><p>Generalized strain or stresses are obtained from complementary strain energy or strain energy, respectively, through:</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x51.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x51.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x52.png" xlink:type="simple"/></inline-formula></p></sec><sec id="s3_2"><title>3.2. Damage According to Thermodynamic Energy</title><p>Based on damage mechanics, thermodynamic strength related to damage <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x53.png" xlink:type="simple"/></inline-formula> is determined, provided by (17), as derived from complementary strain energy, U, related to damage<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x54.png" xlink:type="simple"/></inline-formula>:</p><disp-formula id="scirp.62117-formula784"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-4900380x55.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x56.png" xlink:type="simple"/></inline-formula> is the complementary strain energy of member <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x57.png" xlink:type="simple"/></inline-formula> with A as total transverse area of the element, E as elasticity module, and l the length of the element. N is the axial generalized stress.</p><p>The concept of thermodynamic strength related to damage comes from classical theories of degradation and fracture and may be interpreted as the strength causing damage. Deriving strain energy related to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x58.png" xlink:type="simple"/></inline-formula>, thermodynamic stresses related to plastic generalized strains coincide with generalized strains, which justifies to have considered fluency functions as depending on such.</p></sec></sec><sec id="s4"><title>4. Introduction to Application</title><p>In 1869, James P. Kirkwood, Chief Engineer of the Water Department, St. Louis, USA, described European water plants in a report, which served the American Water Works Association, AWWA as a guide throughout many years to manufacture filters. Many of the first experimental works on slow-action sand filters were carried out at the Lawrence experimental station, Sanity Board, Massachusetts State, USA, which started to operate in November, 1887, and was under supervision of Allen Hazen from summer, 1888, throughout March 1893 [<xref ref-type="bibr" rid="scirp.62117-ref3">3</xref>] . From 1949, Jacobsen researched the dynamic effect of the fluid in aircraft containers, in 1952 Graham and Rodr&#237;guez considered that dynamic pressures of the fluid on the walls may be divided in impulsive and convective pressure. In 1957, Hosner picked up Graham and Rodr&#237;guez’ approach and proposed an analysis procedure based on a simple mass-spring model. In practice, seismic analysis of storage tanks is based on such methodology.</p><p>Mexico City has a population of more than 8,851,080 inhabitants. In 1951, the City required 4 m<sup>3</sup>/s of potable water; and in 1976 it required 9 m<sup>3</sup>/s: this increment was achieved by drilling wells in Lerma Valley [<xref ref-type="bibr" rid="scirp.62117-ref4">4</xref>] - [<xref ref-type="bibr" rid="scirp.62117-ref6">6</xref>] . As water demand increased, water was obtained from a water collection system called Sistema Cutzamala. However, such source has been insufficient. Therefore, the extraction of underground water has become necessary, taking advantage of the fact that Mexico City is seated on a natural basin. Mexico City is subdivided in 16 boroughs. Iztapalapa is the most populated boroughs in the City, with 15,789 inhabitants/km<sup>2</sup> within a 115 km<sup>2</sup> territory, with an inhabitant population projection of 1,850,721 by the year 2015, and a foreseen demand of 8066.42 l/s. Given that it receives 3961.32 l/s, it has an insufficient outflow for the demand.</p><p>Related to the influence of well water components in the corrosion behavior of filtering tanks, <xref ref-type="table" rid="table1">Table 1</xref> shows two heavy metals, iron and manganese, with high influent values: 0.428 mg/l for iron and 0.272 mg/l for manganese. Regarding effluent, the 0.02 mg/l value is lower than the limit, for iron, and 0.01 mg/l higher for manganese, which defines the standard for both cases. In addition, this shows that industrial activity exists in the area where the well is located. Once purification processes and outflow to be potabilized are determined, reinforced concrete, steel or other material is used to construct tanks, sumps, containers, etc. <xref ref-type="fig" rid="fig2">Figure 2</xref> shows location of 16 water treatment plants in the eastern and southern areas in Mexico City, the operation area, as well as the corresponding boroughs.</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Areas in the Federal District for operation of potable water infrastructure. Taken from the Master Potable Water Plan for the Federal District, 1997-2010</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x59.png"/></fig><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Energy U<sub>T</sub> from tensile test and ductility value of steels analyzed</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Steel</th><th align="center" valign="middle" >Energy in elastic area up to ε<sub>y</sub></th><th align="center" valign="middle" >Energy (U<sub>t</sub>) in elastoplastic area between ε<sub>y</sub><sub> </sub>and ε<sub>m&#225;x</sub></th><th align="center" valign="middle" >Energy in damaged area between ε<sub>m&#225;x</sub> and ε<sub>y</sub> limits</th><th align="center" valign="middle" >Strain ε<sub>y</sub></th><th align="center" valign="middle" >Strain ε<sub>m&#225;x</sub></th><th align="center" valign="middle" >Strain ε<sub>u</sub></th><th align="center" valign="middle" >Ductility <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-4900380x60.png" xlink:type="simple"/></inline-formula></th></tr></thead><tr><td align="center" valign="middle" >Not corroded A284 Grade C steel</td><td align="center" valign="middle" >0.3443</td><td align="center" valign="middle" >88.49</td><td align="center" valign="middle" >29.10</td><td align="center" valign="middle" >0.003</td><td align="center" valign="middle" >0.2148</td><td align="center" valign="middle" >0.295</td><td align="center" valign="middle" >53.70</td></tr><tr><td align="center" valign="middle" >Corroded A284 Grade C steel</td><td align="center" valign="middle" >0.25</td><td align="center" valign="middle" >59.60</td><td align="center" valign="middle" >23.27</td><td align="center" valign="middle" >0.0025</td><td align="center" valign="middle" >0.185</td><td align="center" valign="middle" >0.263</td><td align="center" valign="middle" >46.25</td></tr><tr><td align="center" valign="middle" >Not corroded A36 steel</td><td align="center" valign="middle" >0.46</td><td align="center" valign="middle" >37.71</td><td align="center" valign="middle" >22.98</td><td align="center" valign="middle" >0.0025</td><td align="center" valign="middle" >0.078</td><td align="center" valign="middle" >0.124</td><td align="center" valign="middle" >31.2</td></tr><tr><td align="center" valign="middle" >Corroded A36 steel</td><td align="center" valign="middle" >0.35</td><td align="center" valign="middle" >20.97</td><td align="center" valign="middle" >15.04</td><td align="center" valign="middle" >0.0022</td><td align="center" valign="middle" >0.050</td><td align="center" valign="middle" >0.083</td><td align="center" valign="middle" >25.0</td></tr></tbody></table></table-wrap><p>After the first 8 years of operation of the eastern system water treatment plants in Mexico city, 3 out of 10 filters showed exceedingly high corrosion inside the filtering tanks with A284 Grade C steel plates and e = 9.8 mm wall thickness: indeed the corrosion rendered the filters useless. This problem made evident the need to experiment the evolution of corrosion and the structural behavior of the tank damaged by corrosion within the laboratory. Such damage by corrosion generates a local failure in the joint of the false bottom, supporting filtering material, with the wall of the auto-supported tank. Such local failure causes total and/or partial suspension of potabilized water supply to Mexico City. Due to the functioning of such pressurized steel tanks, it is not possible to periodically check the evolution of corrosion inside them: the operation filtering tank would have be suspended, thus affecting potable water supply for up to forty days, i.e. the period required to remove filtering material and properly check false bottom and the wall of the tank.</p><p>We move now to look at the development of the experiment, in order to obtain data related to corrosion in the wall of the damaged filtering tank within a determined period of time; damage analysis, both mechanical and by corrosion; corrosion speed assessment; and discussion of results.</p><sec id="s4_1"><title>4.1. Experimental Development</title><p>Metallographic analysis was carried out to confirm steel used, the corrosion compounds, as well as to determine of the type of damage by corrosion; in A284 Grade C steel with e = 9.8 mm plate thickness used in the hull of the tank and A36 steel with e = 6.35 mm plate thickness used in the reinforcement of the false bottom.</p><p>Six samples of two different thicknesses intervening in the structure of the tank were taken, hull of the tank with 9.8 mm thickness, and a sample of the beams supporting the false bottom inside the tank, 6.35 mm thick, <xref ref-type="fig" rid="fig3">Figure 3</xref>(a) and <xref ref-type="fig" rid="fig3">Figure 3</xref>(b), based on [<xref ref-type="bibr" rid="scirp.62117-ref7">7</xref>] . Dimensions of the sample were 30 &#215; 20 &#215; 9.5 mm and 30 &#215; 20 &#215; 6.35 mm.</p></sec><sec id="s4_2"><title>4.2. Results of Metallographic Analysis</title><p><xref ref-type="fig" rid="fig4">Figure 4</xref>(a) shows the resulting microstructure of “Small Sample” steel pieces (A36 steel, dimensions: 30 &#215; 20 &#215; 6.35 mm) and “Small Sample” (A284 Grade C steel, dimensions: 30 &#215; 20 &#215; 9.52 mm). In the Small Sample</p><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Steel tank damaged by corrosion. (a) Interior of a steel tank under analysis; (b) reinforcement of the false bottom plate. View from below the false bottom.</title></caption><fig id ="fig3_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x61.png"/></fig><fig id ="fig3_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x62.png"/></fig></fig-group><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Microstructure of A36 steel piece. (a) Small sample steel pieces. A36 steel with dimensions: 30 &#215; 20 &#215; 6.35 mm; (b) small sample steel pieces. A284 Grade C steel with dimensions: 30 &#215; 20 &#215; 9.52 mm.</title></caption><fig id ="fig4_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x63.png"/></fig><fig id ="fig4_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x64.png"/></fig></fig-group><p>shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>(b) as M_chica (6) a high quantity of inclusions may be observed, relatively higher than those in sample M_grande (3). M_chica (3) macrograph, obtained by means of secondary electron technique, reveals microstructure of the sample, which includes perlite grains approximately 50 &#181;m - 70 &#181;m long, surrounded by ferrite. This micrography shows that the presence of such inclusions is still evident. Sample M_grande (3) shows a uniform distribution of inclusions in a lower proportion, and less when compared with the Small Sample, which has an approximate interval of 3 &#181;m - 5 &#181;m. Micrography of figure M_grande (3), obtained by means of compositional model technique (retro-dispersed electrons), shows a microstructure with perlite grains 80 &#181;m and 100 &#181;m long, with inclusions.</p><p>Spectrum of <xref ref-type="fig" rid="fig5">Figure 5</xref> shows, separately, elements which, in the corresponding environment, react creating compounds which generate the development of corrosion in the metal. <xref ref-type="fig" rid="fig6">Figure 6</xref> shows the profile of the A284 Grade C steel sample, where damage by corrosion may be observed.</p></sec><sec id="s4_3"><title>4.3. Assessment of Corrosion Speed</title><p>In accordance with results obtained by metallographic analysis, an acceptable 0.2 mm/year corrosion speed is determined for A284 Grade C steel probe, which allows us to consider that, in another 8-year operation period, the structure will also maintain an acceptable corrosion speed, since corrosion compounds generate a passivation</p><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Distribution of chemical elements frequencies conforming metal and corrosion elements (A36 steel)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x65.png"/></fig><fig-group id="fig6"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Microstructure (profile) of A284 Grade C steel named M_grande (3). (a) Corrosion compound and anticorrosion coating debris; (b) depth of generalized corrosion damage.</title></caption><fig id ="fig6_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x66.png"/></fig></fig-group><p>layer controlling and inhibiting corrosion, which allows us to expect proper behavior of structure, even in case of losing the whole coating due to corrosion, as provided by the Rules for Construction in the Federal District, which is 1/6 of calculated plate thickness. In this case, there was a 3 mm increase [<xref ref-type="bibr" rid="scirp.62117-ref8">8</xref>] .</p></sec><sec id="s4_4"><title>4.4. Tensile Strength of Analyzed Steel</title><p>Tensile strength of material is obtained under the stress-strain curve of the tensile test integrated between yield strength and maximum stress (ε<sub>y</sub> and ε<sub>m&#225;x</sub>). Adjusted curve for A284 Grade C not corroded steel provides us with a Degree 5 polynomial, which integration between points ε<sub>y</sub> = 0.0025 and ε<sub>m&#225;x</sub> = 0.2148 shows a 88.495 MPa tensile strength of material, <xref ref-type="fig" rid="fig7">Figure 7</xref>, blue curve. For damaged area between ε<sub>m&#225;x</sub> = 0.2148 and ε<sub>u</sub> = 0.295, energy in the damaged area in the reference probe is: 29.10 MPa, <xref ref-type="fig" rid="fig7">Figure 7</xref>, blue curve. For not corroded A284 Grade C steel, tensile strength U<sub>t</sub> of not corroded A284 Grade C steel is: 59.60 MPa, <xref ref-type="fig" rid="fig7">Figure 7</xref>, red curve. For the damaged area, there is a Degree 4 polynomial, and the value of energy in the damaged area is 28.273 MPa, <xref ref-type="fig" rid="fig7">Figure 7</xref>, red curve.</p></sec><sec id="s4_5"><title>4.5. Not Corroded A36 Steel</title><p>For not corroded A36 steel, there is a Degree 6 polynomial with limits: ε<sub>y</sub> = 0.0030, ε<sub>m&#225;x</sub> = 0.078 and 37.26 MPa tensile strength U<sub>t</sub>, <xref ref-type="fig" rid="fig8">Figure 8</xref>, blue curve. Energy (equal to the area under the stress-strain curve for not corroded</p><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> A284 Grade C Steel. (a) Tensile strength calculation for reference not corroded probe; (b) energy calculation in damaged area for reference not corroded probe; (c) tensile strength calculation for corroded probe; and (d) energy calculation in damaged area for corroded probe</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x67.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> A36 Steel. (a) tensile strength calculation for reference not corroded probe; (b) energy calculation in damaged area for reference not corroded probe; (c) tensile strength calculation for corroded probe; and (d) energy calculation in damaged area for corroded probe</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x68.png"/></fig><p>A36 steel damaged area) is obtained integrating a Degree 4 polynomial to data between ε<sub>m&#225;x</sub> = 0.080 and ε<sub>u</sub> = 0.124 limits, <xref ref-type="fig" rid="fig8">Figure 8</xref>, blue curve, providing us with a 22.98 MPa value.</p></sec><sec id="s4_6"><title>4.6. Corroded A36 Steel</title><p>Tensile strength of corroded A36 steel, based on a Degree 5 polynomial, is 20.97 MPa, <xref ref-type="fig" rid="fig8">Figure 8</xref>, in green. Energy in damaged area for corroded A36 steel is: 15.045 MPa, shown in <xref ref-type="fig" rid="fig8">Figure 8</xref>, in green. <xref ref-type="table" rid="table1">Table 1</xref> shows data for energy U<sub>T</sub> from the tensile test, as well as ductility value of analyzed steels in the three areas for both steels.</p><p>For A284 Grade C steel, a 925.8 (N∙m) maximum value has been observed for a 0.9 damage, which shows higher ductility of A284 Grade C steel, while for corroded probe, a 531.93 (N∙m) maximum value has been obtained for a 0.9 damage, 57% energy of not corroded probe in accord to (17). For A36 steel, a 358 (N∙m) the maximum value has been observed for a 0.9 damage, and a 284.067 (N∙m) value for a 0.9 damage in the corroded probe, representing 79% energy of not corroded probe.</p></sec></sec><sec id="s5"><title>5. Discussion of Results</title><p>Heavy metal concentrations are indicators of the damaging and corrosion process already present in the tank, and the gradual detachment of metals in the inside. For influent, such concentrations may be due to damaging and corrosion process of pipes feeding the well. This shows that, in effect, the corrosion process occurs in 5 phases. In our case, the first phase is related to the effluent effect; the second one is transition of humidity excess effect; the third one is first phase of corrosion effect; the fourth one is transition of corrosion effect; and the fifth and last one is stabilization of corrosion effect [<xref ref-type="bibr" rid="scirp.62117-ref9">9</xref>] .</p><p>Yield strength determined for A284 Grade C steel in the reference probe, was 295 MPa (3000 kg/cm<sup>2</sup>), very close to the theoretical 290 MPa (2950 kg/cm<sup>2</sup>) value. The stress value for corroded steel was 237 MPa (2416 kg/cm<sup>2</sup>). It can be considered that A284 Grade C steel underwent a 19.5% yield strength loss. As <xref ref-type="fig" rid="fig9">Figure 9</xref> shows, such difference has low influence on structural behavior of steel, since a maximum allowable stress equal to 2/3 of yield strength , 193 MPa (1966 kg/cm<sup>2</sup>), was taken into consideration in the design of structural elements, in this case, of the hull of the tank. Acting stresses are even lower, which is confirmed in view of radial displacements of hull of the tank, taking into consideration loss of thickness due to corrosion.</p><p>In the test carried out on A36 steel, yield strength value for non-corroded steel was determined as 368 MPa (3750 kg/cm<sup>2</sup>), the theoretical value for such stress is 345 MPa (3500 kg/cm<sup>2</sup>) and the value determined in test for corroded steel is 312 MPa (3181 kg/cm<sup>2</sup>). It was determined that steel lost 15.5% stress yield strength, as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>0. The structural element designed with such steel is the false bottom support for filtering material inside the steel tank. Such element is an “I” profile with plate, including the false bottom plate as higher skid. Such type of profile is more sensible to plate thickness loss due to corrosion.</p><p>A284 Grade C steel shows a 32% decrease of energy in elastoplastic area, while A 36 steel shows a 35% decrease of energy in this area, <xref ref-type="table" rid="table1">Table 1</xref>. This is due to higher ductility of A284 Grade C steel, which has a 13.88% ductility loss due to corrosion after 8 years of operation. A36 steel has a 17.5% ductility loss, in the same period, that is, it loses more ductility due to the composition of steel.</p><p>An ultimate 925.8 (N∙m) value for 0.9 damage has been observed for A284 Grade C steel. This shows higher ductility of A284 Grade C steel. An ultimate 358 (N∙m) value for 0.9 damage has been observed for A36 steel, due to lower ductility of such steel.</p><p>Upon tank examination, determination of minimal thickness of tank was found to be adequate, where internal pressure determines thickness and, since the formula does not take into consideration coating to prevent corro-</p><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Yield strength stress comparison between corroded and not corroded A284 Grade C steel</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x69.png"/></fig><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> Yield strength stress comparison between corroded and not corroded A36 steel</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-4900380x70.png"/></fig><p>sion, the corresponding standard [<xref ref-type="bibr" rid="scirp.62117-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.62117-ref11">11</xref>] , requires the addition of 1/6 of determined thickness, thus obtaining a proper safety level. This has been verified since, after 8 years of operation, steel showed generalized corrosion with a corrosion speed classified as good, being between 0.1 and 0.5 mm/year.</p><p>Stresses on the tangent line below the hull of the tank under analysis are 365.25 kg/cm<sup>2</sup>. With stress combination due to a seismic event, the most adverse one, such stress increases up to 574.31 kg/cm<sup>2</sup>, this being half the maximum allowable 1165 kg/m<sup>2</sup> stress, and corrosion does not imply an increase in stress, since the thickness increase to prevent corrosion is three times higher due to the corrosion loss shown in such period of time. In the design of false bottom and “I” profile supporting such, it was found that such profile is more sensible to variation of thickness in such section. Therefore, it shows an increase of stress where, due to thickness loss caused by corrosion, cutting stress increases from f<sub>v</sub> = 1042 kg/cm<sup>2</sup> up to f<sub>v</sub> = 1403 kg/cm<sup>2</sup>, thus going beyond the allowable FV stress, even with reinforcement in both directions.</p></sec><sec id="s6"><title>6. Conclusions</title><p>The theoretical development of damage analysis presented allows understanding the loss of strength phenomenon in metals caused by combined mechanical and electro-chemical corrosion damage effects. A-284 Grade C steel had a higher strength loss measured as fluency stress compared to loss of A-36 steel. The carbon content in steel composition influences variation of strength loss. Steel with higher carbon content has a lower fluency stress and shall also have a higher strength or fluency stress loss due to its higher ductility.</p><p>Local failure of false bottom in the filtration tank is due to cracks in tubular connections, since such are areas of high concentration of stresses and high residual stresses. In addition, in those areas the presence of defects in welding is very common. Cathode protection must be considered in the design of such filtration tanks, placing anodes in sections where corrosion is more severe. In our case, it is the joint of the hull with the false bottom.</p><p>Carbon steels show, in general, a micro-structure composed by ferrite and perlite, in normal state, as they leave the plant. Grains of material are oriented towards the lamination direction. Among these grains, a flat dislocations distribution prevails. Such dislocations grow as carbon content increases. The metallographic study of the two steels analyzed determined that there are no dislocations of material in their composition which may be considered as a factor of size increasing continuous damage.</p><p>The passivation phenomenon in analyzed steel may be considered, since creation of a protecting surface layer of corrosion products such as iron oxide and other ferrous composites derived from anticorrosion coating used in the manufacture of the tank, inhibits dissolution reactions of the metal. This could be observed with the scanning electron microscope.</p><p>The benefits of adopting a predictive maintenance strategy would benefit in knowing integrity degree of the inside of the tank, and the joint of the false bottom with the wall of the tank, which may be achieved only draining the tanks and coming into such. Some additional benefits would be extending the useful life of the tank, increasing safety and reducing maintenance costs.</p></sec><sec id="s7"><title>Acknowledgements</title><p>This document was developed with part of the time devoted to the IPN-SIP 20120585 research project.</p></sec><sec id="s8"><title>Cite this paper</title><p>FranciscoCasanova-del-Angel,Mois&#233;sGayt&#225;n-L&#243;pez, (2015) Analytical Model on Steel Tanks Damaged by Corrosion. World Journal of Mechanics,05,274-285. doi: 10.4236/wjm.2015.512026</p></sec></body><back><ref-list><title>References</title><ref id="scirp.62117-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Bolotin, V.V. and Shipkov, A.A. (2001) Mechanical Aspects of Corrosion Fatigue and Stress Corrosion Cracking. International Journal of Solids and Structures, 38, 7297-7318.</mixed-citation></ref><ref id="scirp.62117-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Gérard, B., Pijaudier-Cabot, G. and La Borderie, C. (1998) Coupled Diffusion-Damage Modelling and the Implications on Failure Due to Strain Localisation. International Journal of Solids and Structures, 35, 4107-4120.</mixed-citation></ref><ref id="scirp.62117-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Fair, G.M., Geyer, J.C. and Okun, D.A. (1979) Purificación de agua y tratamiento y remoción de aguas residuals. Volumen II. Editorial LIMUSA. México.</mixed-citation></ref><ref id="scirp.62117-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">DGCOH (1997-1) Elaboración de anteproyectos para solucionar los problemas de suministro de agua en diversas colonias de la Delegación Iztapalapa. Consultoría en Ingeniería Itzana S.A. de C.V. Dirección Técnica, Subdirección de Programación. U.D. Planes Hidráulicos Delegacionales. Dirección General de Construcción y Operación Hidráulica. Secretaría de Obras y Servicios. GDF. México.</mixed-citation></ref><ref id="scirp.62117-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">DGCOH (1997-2) Diagnóstico de la problemática de suministro de agua potable y drenaje en la Delegación Iztapalapa. Automatizaciones y proyectos de Ingeniería S.A. de C.V. Dirección General de Construcción y Operación Hidráulica. Secretaría de Obras y Servicios. GDF. México.</mixed-citation></ref><ref id="scirp.62117-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">DGCOH (1995) Criterio para sancionar la calidad de agua potable. Dirección General de Construcción y Operación Hidráulica. Secretaría de Obras y Servicios. DDF. México.</mixed-citation></ref><ref id="scirp.62117-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">ASTM (American Society of Testing Material) Designation: E8-01 (2002) Standard Test Methods for Tension Testing of Metallic Materials.</mixed-citation></ref><ref id="scirp.62117-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">RCDF (2004) Reglamento de Construcciones para el Distrito Federal. GDF. México.</mixed-citation></ref><ref id="scirp.62117-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">Casanova-del-Angel, F. and Toquiantzi Butrón, R. (2008) Corrosion Phases of Structural Shapes Exposed to the Atmosphere. Corrosion Science, 50, 2288-2295.  
http://dx.doi.org/10.1016/j.corsci.2008.05.015</mixed-citation></ref><ref id="scirp.62117-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">Standard API 620 (1990) Para tanques de almacenamientos sometidos a presiones internas cercanas a 1 kg/cm2.</mixed-citation></ref><ref id="scirp.62117-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">Standard API 650 (1998) Aplicable a grandes tanques horizontales o verticales soldados en campo y presión de operación menores de 1 Kg/cm2.</mixed-citation></ref></ref-list></back></article>