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	<front>
		<journal-meta>
			<journal-id journal-id-type="publisher-id">REVMET</journal-id>
			<journal-title-group>
				<journal-title>Revista de Metalurgia</journal-title>
				<abbrev-journal-title abbrev-type="publisher">REVMETAL</abbrev-journal-title>
			</journal-title-group>
			<issn publication-format="electronic">1988-4222</issn>
			<issn-l>0034-8570</issn-l>
			<publisher>
				<publisher-name>Consejo Superior de Investigaciones Cient&#xed;ficas</publisher-name>
			</publisher>
		</journal-meta>
		<article-meta>
			<article-id pub-id-type="publisher-id">revmetalm.185</article-id>
			<article-id pub-id-type="doi">10.3989/revmetalm.185</article-id>
			<article-categories>
				<subj-group subj-group-type="heading">
					<subject>Articles</subject>
				</subj-group>
			</article-categories>
			<title-group>
				<article-title>Investigation of mechanical and corrosion properties of Al 7075/Redmud metal matrix composite</article-title>
				<trans-title-group xml:lang="es">
					<trans-title>Investigaci&#xf3;n sobre las propiedades mec&#xe1;nicas y de corrosi&#xf3;n del compuesto de matriz met&#xe1;lica Al 7075/Redmud</trans-title>
				</trans-title-group>
			</title-group>
			<contrib-group>
				<contrib contrib-type="author" corresp="yes">
					<contrib-id contrib-id-type="orcid">https://orcid.org/0000-0003-2607-3454</contrib-id>
					<name>
						<surname>Sambathkumar</surname>
						<given-names>Mani</given-names>
					</name>
					<email xlink:href="sambathme@gmail.com">sambathme@gmail.com</email>
					<aff id="aff1"><institution>Department of Mechanical Engineering, Kongu Engineering College</institution>, <addr-line>Erode, Tamilnadu</addr-line>, <country>India</country></aff>
				</contrib>
				<contrib contrib-type="author">
					<contrib-id contrib-id-type="orcid">https://orcid.org/0000-0002-0107-3442</contrib-id>
					<name>
						<surname>Sasikumar</surname>
						<given-names>Kondayampalayam S.K.</given-names>
					</name>
					<aff id="aff2"><institution>Department of Mechanical Engineering, Kongu Engineering College</institution>, <addr-line>Erode, Tamilnadu</addr-line>, <country>India</country></aff>
				</contrib>
				<contrib contrib-type="author">
					<contrib-id contrib-id-type="orcid">https://orcid.org/0000-0001-9924-4440</contrib-id>
					<name>
						<surname>Gukendran</surname>
						<given-names>Rangasamy</given-names>
					</name>
					<aff id="aff3"><institution>Department of Mechanical Engineering, Kongu Engineering College</institution>, <addr-line>Erode, Tamilnadu</addr-line>, <country>India</country></aff>
				</contrib>
				<contrib contrib-type="author">
					<contrib-id contrib-id-type="orcid">https://orcid.org/0000-0001-8355-6175</contrib-id>
					<name>
						<surname>Dineshkumar</surname>
						<given-names>Karupannasamy</given-names>
					</name>
					<aff id="aff4"><institution>Department of Mechanical Engineering, Kongu Engineering College</institution>, <addr-line>Erode, Tamilnadu</addr-line>, <country>India</country></aff>
				</contrib>
				<contrib contrib-type="author">
					<contrib-id contrib-id-type="orcid">https://orcid.org/0000-0002-7327-0365</contrib-id>
					<name>
						<surname>Ponappa</surname>
						<given-names>Kannayiram</given-names>
					</name>
					<aff id="aff5"><institution>Department of Mechanical Engineering, Indian Institute of Information Technology Design and Manufacturing Jabalpur</institution>, <addr-line>Jabalpur</addr-line>, <country>India</country></aff>
				</contrib>
				<contrib contrib-type="author">
					<contrib-id contrib-id-type="orcid">https://orcid.org/0000-0003-2120-2421</contrib-id>
					<name>
						<surname>Harichandran</surname>
						<given-names>Samiyappan</given-names>
					</name>
					<aff id="aff6"><institution>Department of Mechanical Engineering, Kongu Engineering College</institution>, <addr-line>Erode, Tamilnadu</addr-line>, <country>India</country></aff>
				</contrib>
			</contrib-group>
			<pub-date pub-type="epub">
				<day>01</day>
				<month>03</month>
				<year>2021</year>
			</pub-date>
			<pub-date pub-type="collection">
				<month>03</month>
				<year>2021</year>
			</pub-date>
			<volume>57</volume>
			<issue>1</issue>
			<elocation-id>e185</elocation-id>
			<history>
				<date date-type="received">
					<day>09</day>
					<month>04</month>
					<year>2020</year>
				</date>
				<date date-type="accepted">
					<day>18</day>
					<month>01</month>
					<year>2021</year>
				</date>
				<date date-type="pub">
					<day>07</day>
					<month>04</month>
					<year>2021</year>
				</date>
			</history>
			<permissions>
				<copyright-statement>&#xa9;2021 CSIC</copyright-statement>
				<copyright-year>2021</copyright-year>
				<license license-type="open-access" xlink:href="https://creativecommons.org/licenses/by/4.0/">
					<license-p>This is an open-access article distributed under the terms of the Creative Commons Attribution 4.0 International (CC BY 4.0) License.</license-p>
				</license>
			</permissions>
			<self-uri xlink:href="http://revistademetalurgia.revistas.csic.es/index.php/revistademetalurgia/article/view/XXXX/XXXX"/>
			<abstract>
				<title>Abstract</title>
				<p>Investigation in this paper is mechanical properties and corrosion properties of Al 7075 metal matrix composites. Al 7075 metal matrix composite is prepared from Al 7075 as a matrix and redmud as a reinforcement by using two step stir casting process. Volume percentage of reinforcement is varied from 0&#x25; to 15&#x25;. The experimental density of the composite material produced was calculated according to the Archimedes principle, greater than the basic matrix. Uniform distribution of the reinforcement and matrix in the composite is studied by using optical micrographs and microhardness of the composite is measured by using Vickers hardness testing machine. The microhardness of the composite was increased while the reinforcement went from 0&#x25; to 15&#x25;. The tensile strength of the composite material is raised at 5&#x25; of the reinforcement tolerance (326 MPa), which is higher than the base matrix. The Al 7075 metal matrix composites have a lower corrosion rate in a 3.5&#x25; NaCl solution than the base matrix. As the volume percentage increase in red mud, was reduced the corrosion rate of the composites.</p>
			</abstract>
			<trans-abstract xml:lang="es">
				<title>Resumen</title>
				<p>En el presente trabajo se realiza una investigaci&#xf3;n sobre las propiedades mec&#xe1;nicas y el comportamiento frente a corrosi&#xf3;n del compuesto de matriz met&#xe1;lica Al 7075. El cual se prepar&#xf3; a partir de Al 7075 como matriz y lodo rojo como refuerzo, mediante el uso de un proceso de fundici&#xf3;n por agitaci&#xf3;n en dos pasos. El porcentaje en volumen de refuerzo var&#xed;a de 0&#x25; a 15&#x25;. La densidad del material compuesto se calcul&#xf3; mediante el principio de Arqu&#xed;medes, mayor que la matriz b&#xe1;sica. La distribuci&#xf3;n uniforme del refuerzo y la matriz en el material compuesto se estudi&#xf3; utilizando micrograf&#xed;as &#xf3;pticas, y la microdureza del material se determin&#xf3; utilizando una m&#xe1;quina de ensayo de dureza Vickers. La microdureza del compuesto aument&#xf3;, mientras que el refuerzo pas&#xf3; del 0&#x25; al 15&#x25;. La resistencia a la tracci&#xf3;n del material compuesto se elev&#xf3; al 5&#x25; de la tolerancia de refuerzo (326 MPa), que es m&#xe1;s alta que la matriz base. Los compuestos de matriz met&#xe1;lica Al 7075 presentan una velocidad de corrosi&#xf3;n m&#xe1;s baja en una soluci&#xf3;n de NaCl al 3,5&#x25; que la matriz base. A medida que aumenta el porcentaje en volumen en el lodo rojo, se reduce la velocidad de corrosi&#xf3;n de los compuestos.</p>
			</trans-abstract>
			<kwd-group>
				<kwd>Al 7075</kwd>
				<kwd>Corrosion properties</kwd>
				<kwd>Mechanical Properties</kwd>
				<kwd>Redmud</kwd>
				<kwd>Stir casting</kwd>
				<kwd>Two-step</kwd>
			</kwd-group>
			<kwd-group xml:lang="es">
				<kwd>Al 7075</kwd>
				<kwd>Lodo rojo</kwd>
				<kwd>Fundici&#xf3;n por agitaci&#xf3;n en dos pasos</kwd>
				<kwd>Propiedades frente a la corrosi&#xf3;n</kwd>
				<kwd>Propiedades mec&#xe1;nicas</kwd>
			</kwd-group>
			<counts>
				<fig-count count="6"/>
				<table-count count="7"/>
				<equation-count count="0"/>
				<ref-count count="26"/>
				<page-count count="9"/>
			</counts>
		</article-meta>
	</front>
	<body>
		<sec id="sec1" sec-type="intro">
			<label>1.</label>
			<title>Introduction</title>
			<p>In recent times aluminium alloys play a major role in composite preparation. There are N no. of combination available in aluminium alloys, they are Al7075, Al6061, Al2024, Al8081, Al6063, A413, A380, A356, A535, etc. This is the reason why researchers move to aluminium composites. Due to its high strength to density ratio, high tensile strength, high yield strength and its high elongation during downtime is the reason for Al7075 has a large number of applications in the automotive, aerospace, machine and ship industries (<xref ref-type="bibr" rid="B7">Baradeswaran and Perumal, 2014a</xref>; <xref ref-type="bibr" rid="B8">Baradeswaran and Perumal, 2014b</xref>; <xref ref-type="bibr" rid="B14">Imran <italic>et al.</italic>, 2016</xref>; <xref ref-type="bibr" rid="B11">Devaganesh <italic>et al.</italic>, 2020</xref>; <xref ref-type="bibr" rid="B1">Alaneme <italic>et al.,</italic> 2020</xref>; <xref ref-type="bibr" rid="B9">&#xc7;avdar <italic>et al.</italic>, 2020</xref>) There are various methods for producing the particles reinforced MMC, including stir casting is one of the best method for production of MMC. Casting is very popular because of its simplicity and flexibility and is the most economical method for the production of large components (<xref ref-type="bibr" rid="B21">Sambathkumar <italic>et al.</italic>, 2017</xref>; <xref ref-type="bibr" rid="B22">Sharma <italic>et al.</italic>, 2018</xref>). Composites consist of one or more discontinuous phases that are integrated in a continuous phase. The discontinuous phase is generally harder and stronger than the continuous phase and is called a reinforcing material, the continuous phase is called a matrix. The main function is to transfer and distribute the load to the fiber reinforcement. The matrix can be selected based on its resistance to oxidation and corrosion. Metallic matrix Composite materials (MMC) offer designers advantages, they are particularly suitable for applications good resistance to high temperatures, good structural rigidity, dimensional stability, and light (<xref ref-type="bibr" rid="B18">Prasad <italic>et al.</italic>, 2013</xref>). Red mud is one of the main wastes in the production of aluminium oxide from bauxite using the Bayer process. It is an insoluble product that is produced after the digestion of bauxite with sodium hydroxide at high temperature and pressure and is known as red mud or “bauxite residue”. It contains oxides of iron, titanium, aluminium and silica as well as other secondary components. Due to economic and ecological issues, enormous efforts have been made worldwide to solve problems of red mud management, i.e., the use, storage and disposal (<xref ref-type="bibr" rid="B17">Pradeep <italic>et al.</italic>, 2014</xref>). </p>
			<p>Corrosion can affect the metal matrix composite in several ways, depending on its nature and the prevailing environmental conditions. Examination of the corrosion resistance of Al-based materials is important, especially for automotive and aerospace applications where the parts are exposed to corrosive media such as salt water solutions, acidic and alkaline media. The main advantages of AMMC compared to unreinforced materials are as follows: higher strength, improved rigidity, reduced density, good corrosion resistance, improved properties at high temperature, coefficient of controlled thermal expansion, thermal/thermal management, resistance to improved wear and improved damping capacities. Aluminium 6061-MMC with a volume percentage of 0 to 6 percent reinforced with red mud particles has been successfully manufactured using liquid molten metallurgy technology. The corrosion rate of the alloy and the composite material decreased with increasing time in seawater. The corrosion rate of the composite materials was lower than that of the corresponding matrix alloy in seawater Composite materials are better suited to marine environments than matrix alloys (<xref ref-type="bibr" rid="B15">Krupakara and Ravikumar, 2015</xref>). It has also been observed that the addition of red mud under the current test conditions results are increase in hardness and a decrease in the yield strength and electrical conductivity. Here it is observed that as the size of the red mud particles decreases, the density, hardness, yield strength and electrical conductivity of the sintered compacts gradually increases (<xref ref-type="bibr" rid="B20">Sai, 2014</xref>). Red mud, the waste from the Production of alumina, has been used successfully as reinforcement material based on an aluminium alloy Composites with better wear resistance. These composite materials can be used instead of the classic ones Aluminium-based alloys. Composites can replace expensive reinforcement materials like, SiC and Al<sub>2</sub>O<sub>3</sub> with red mud, which leads to Reduce costs and use industrial waste (<xref ref-type="bibr" rid="B24">Singla <italic>et al.</italic>, 2015</xref>). The results show that the specific wear rate of the composite increases with increasing temperature. The reason for an increase in the wear rate at high temperature may be a loss of wear resistance at high temperature by softening the matrix (<xref ref-type="bibr" rid="B10">Dabral <italic>et al.</italic>, 2017</xref>). Heat treated Al 6061/red mud composites improved the surface property like reduction of the cracks on surfaces (<xref ref-type="bibr" rid="B16">Panwar <italic>et al.,</italic> 2020</xref>). Addition of cermet (WC-Co) in to the Al 7075 matrix improves the hardness around 10.52&#x25;. The cermet particles also improve yield strength (49&#x25;) and tensile strength (58&#x25;) of the Al 7075 composite (<xref ref-type="bibr" rid="B13">Guruchannabasavaiah <italic>et al.</italic>, 2021</xref>). Samples of the Al 7075 hybrid metal matrix composites are fabricated by two step stir casting process. Theoretical densities are calculated by using rule of mixture concept and experimental densities are calculated by using Archimedes principle. Phases of the composite was analyzed by using the method X-Ray diffraction (XRD) in Rigaku Ultima IV. Hardness of the composite is measured by using Vickers hardness tester in the standard of <xref ref-type="bibr" rid="B3">ASTM E384-11 (2011)</xref> by using diamond indenter. Microstructure of the composites are studied by using the optical photomicrographs. Tensile test of the specimen is carried out by using universal tensile testing machine in the standard of <xref ref-type="bibr" rid="B5">ASTM E8/E8M-13a (2013)</xref>. Corrosion test for the composite is done with 3.5&#x25; NaCl solution by using potentiodynamic polarization method. Finally studied the fractography and severity of corrosion by using SEM (<xref ref-type="bibr" rid="B21">Sambathkumar <italic>et al.</italic>, 2017</xref>). Addition of 15wt.&#x25; of SiC particles into the matrix improved the composite hardness and also showed better wear resistance compared to base alloy. Percentage of SiC and load play a significant role in the wear loss and coefficient of friction (<xref ref-type="bibr" rid="B25">Surya and Prasanthi, 2021</xref>).</p>
			<p>The samples were subjected to wear and mechanical properties tests according to ASTM standards. It has been found that the microhardness, tensile strength, compressive strength and impact resistance of smaller composites have been increased Red mud particles were added to the composite (<xref ref-type="bibr" rid="B12">Geetha and Ganesan, 2019</xref>). The addition of graphite to an aluminium alloy is known to reduce hardness, tensile strength, compressive strength and flexural strength, and has been overcome by the addition of Al<sub>2</sub>O<sub>3</sub> in hybrid composites. The presence of graphite in the hybrid composites has shown a tendency to maintain wear, less due to the formation of a thin layer of graphite on the surface of the tribo (<xref ref-type="bibr" rid="B8">Baradeswaran and Perumal, 2014b</xref>). Corrosion tests were carried out according to ASTM standards. A salt spray test using NaCl was carried out according to <xref ref-type="bibr" rid="B6">ASTM B117-19 (2019)</xref> and immersion tests using NaCl and NaOH as corrodents were carried out according to <xref ref-type="bibr" rid="B4">ASTM G31-12a (2012)</xref> standards (<xref ref-type="bibr" rid="B19">Ravi Kumar <italic>et al.</italic>, 2018</xref>). In a two-step stir casting method, the structural defects such as wettability, interfacial reactions, particle cluster, porosity and oxide inclusions were overcome compared to the conventional casting technique (<xref ref-type="bibr" rid="B26">Zhou and Xu, 1997</xref>; <xref ref-type="bibr" rid="B2">Aravindan <italic>et al.</italic>, 2015</xref>). </p>
			<p>Based on the literature survey, studies on mechanical and corrosion behaviour of Al 7075 composite reinforced with (5, 10, 15 Vol. &#x25;) red mud particle is not available. The main objective of the present study is to fabricate of Al7075/red mud composites and to investigate their mechanical and corrosion behaviour.</p>
		</sec>
		<sec id="sec2" sec-type="materials|methods">
			<label>2.</label>
			<title>Materials and methods</title>
			<p>The base matrix is Al 7075 and the reinforcement material is Redmud for this present study of different composition of metal matrix composite. The chemical composition of the matrix and the properties of the matrix and the reinforcements are given in <xref ref-type="table" rid="t1">Table 1</xref> and <xref ref-type="table" rid="t2">Table 2</xref>. Samples of the metal matrix composites are made using the two-stage stir casting technique. The amounts of matrix material and reinforcements were determined by calculating the volume percentages. </p>
			<table-wrap id="t1">
				<label>Table 1</label>
				<caption>
					<title>Chemical Composition of Al7075 by volume percentage</title>
				</caption>
				<table>
					<colgroup>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
					</colgroup>
					<thead>
						<tr>
							<th align="left">Chemical Composition</th>
							<th align="left">Si</th>
							<th align="left">Fe</th>
							<th align="left">Cu</th>
							<th align="left">Mn</th>
							<th align="left">Mg</th>
							<th align="left">Cr</th>
							<th align="left">Zn</th>
							<th align="left">Ti</th>
							<th align="left">Al</th>
						</tr>
					</thead>
					<tbody>
						<tr>
							<td align="left">Al 7075</td>
							<td align="left">0.4</td>
							<td align="left">0.5</td>
							<td align="left">1.6</td>
							<td align="left">0.3</td>
							<td align="left">2.5</td>
							<td align="left">0.15</td>
							<td align="left">5.5</td>
							<td align="left">0.2</td>
							<td align="left">Rest</td>
						</tr>
					</tbody>
				</table>
			</table-wrap>
			<table-wrap id="t2">
				<label>Table 2</label>
				<caption>
					<title>Properties of matrix and reinforcement material</title>
				</caption>
				<table>
					<colgroup>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
					</colgroup>
					<thead>
						<tr>
							<th align="center">Properties</th>
							<th align="center">Density g·cm<sup>-3</sup>
							</th>
							<th align="center">Specific gravity g·cm<sup>-3</sup>
							</th>
							<th align="center">Hardness</th>
							<th align="center">Tensile strength MPa</th>
							<th align="center">Poisson’s ratio</th>
							<th align="center">PH value</th>
							<th align="center">Particle size</th>
						</tr>
					</thead>
					<tbody>
						<tr>
							<td align="left">AL 7075</td>
							<td align="center">2.81</td>
							<td align="center">2.73</td>
							<td align="center">60 (HB500)</td>
							<td align="center">220</td>
							<td align="center">0.33</td>
							<td align="center">-</td>
							<td align="center">-</td>
						</tr>
						<tr>
							<td align="left">REDMUD</td>
							<td align="center">3.26</td>
							<td align="center">2.77</td>
							<td align="center">-</td>
							<td align="center">-</td>
							<td align="center">-</td>
							<td align="center">10-13</td>
							<td align="center">6 &#xb5;m</td>
						</tr>
					</tbody>
				</table>
			</table-wrap>
			<p>The configuration of the stirring of moulding process consists of the furnace, the fire resistance stirring motor and the speed controller. The melting was carried out in the oven at 700 &#xb0;C and the stirring was completed using a stirring motor and a speed controller. This setup is showen in <xref ref-type="fig" rid="f1">Fig. 1a</xref>. The Redmud was preheated before being added to the aluminium matrix. The aluminium material was first heated to complete melting above the temperature of the liquid and converted to liquid form. It was then cooled below the liquid temperature to keep the molten metal in a semi-solid state. The preheated reinforcement (Redmud) was placed in the molten metal and stirred manually. The oven was then turned on to return the molten mixture to the liquid state. This was stirred mechanically for about 10 to 15 min at an average stirring speed of 150 to 200 rpm. The final temperature was maintained at 750 &#xb0;C &#xb1; 100 &#xb0;C. </p>
			<p>Finally, the molten metal matrix composite was transferred to a metal of die. The die is made of mild steel with dimensions 150 x 60 x 50 mm<sup>3</sup>. Volume &#x25; of the matrix and the reinforcement in the metal matrix composite are shown in <xref ref-type="table" rid="t3">Table 3</xref>. The die used for preparing composite and produced composites are illustrated in <xref ref-type="fig" rid="f1">Fig. 1 (b and c)</xref>.</p>
			<table-wrap id="t3">
				<label>Table 3</label>
				<caption>
					<title>Volume &#x25; of matrix and reinforcement material</title>
				</caption>
				<table>
					<colgroup>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
					</colgroup>
					<thead>
						<tr>
							<th align="left">S.No.</th>
							<th align="left">1</th>
							<th align="left">2</th>
							<th align="left">3</th>
							<th align="left">4</th>
						</tr>
						<tr>
							<th align="left">NAME</th>
							<th align="left">ALR0</th>
							<th align="left">ALR5</th>
							<th align="left">ALR10</th>
							<th align="left">ALR15</th>
						</tr>
					</thead>
					<tbody>
						<tr>
							<td align="left">Vol. &#x25; of AL 7075</td>
							<td align="left">100</td>
							<td align="left">95</td>
							<td align="left">90</td>
							<td align="left">85</td>
						</tr>
						<tr>
							<td align="left">Vol. &#x25; of Redmud</td>
							<td align="left">0</td>
							<td align="left">5</td>
							<td align="left">10</td>
							<td align="left">15</td>
						</tr>
					</tbody>
				</table>
			</table-wrap>
			<fig id="f1">
				<label>Figure 1</label>
				<caption>
					<title>(a) Stir casting setup, (b) Die, (c) Fabricated metal matrix composite, (d) Tensile specimens before testing and (e) Tensile specimens after testing</title>
				</caption>
				<graphic id="gra-1" xlink:href="REVMET-57-01-e185-gf1.png"/>
			</fig>
			<p>Archimedes’ principle was used to calculate the experimental density and the mixing rule to calculate the theoretical density. The porosity of the composites produced is calculated using the theoretical and experimental densities calculated. The Vickers microhardness of the composites produced is measured using a Wilson microhardness tester. The Vickers microhardness of the cast base material Al 7075 and its composites (ALR0, ALR5, ALR10, ALR15) was determined according to <xref ref-type="bibr" rid="B3">ASTM standard E384-11 (2011)</xref> using a diamond penetrator with an applied load of 500 g with a time of 10 s nominal stay. The microstructure of the polished and mirror polished samples is examined using an inverted metallurgical microscope to obtain optical microphotographs.</p>
			<p>The samples are prepared for tensile tests in accordance with <xref ref-type="bibr" rid="B5">ASTM E8/E8M-13a (2013)</xref> as shown in <xref ref-type="fig" rid="f1">Fig. 1d</xref>. These samples are tested in the universal tensile testing machine (Instron) at an elongation speed of 1 mm/min. Seven tensile test pieces were tested and the mean value of the tensile strength of each pieces was shown graphically. <xref ref-type="fig" rid="f1">Figure 1e</xref> each shows the tensile test pieces tested. Tensile test provides different kind of results they are, peak load, elongation and Ultimate tensile strength.</p>
		</sec>
		<sec id="sec3" sec-type="results|discussion">
			<label>3.</label>
			<title>Results and discussion</title>
			<sec id="sec3.1">
				<label>3.1.</label>
				<title>Density and porosity</title>
				<p>The theoretical density of the metal matrix composite produced was calculated using the concept called as rule of mixture. The experimental density of this composite was measured using the principle of Archimedes. The porosity of the composite was calculated using theoretical and experimental densities. Porosity or void proportion is a measure of voids in a material. These values obtained are presented in <xref ref-type="table" rid="t4">Table 4</xref>. During the analysis of <xref ref-type="table" rid="t4">Table 4</xref>, it can be observed that the theoretical and experimental density and porosity of the composites are higher than the base matrix Al 7075. The theoretical, experimental values of density and porosity of the composites are increased while increasing the Vol. &#x25; of the reinforcement during the stirring casting process. The reason for the increased porosity is the formation of pores on the surfaces of the reinforcing particles. This increases the generation of gas bubbles and the flow of liquid metal in the composite materials. The maximum permissible degree of porosity for die-cast aluminium composite materials is within the limit of 4&#x25;.</p>
				<table-wrap id="t4">
					<label>Table 4</label>
					<caption>
						<title>Comparison of theoretical, experimental density and porosity of the composites</title>
					</caption>
					<table>
						<colgroup>
							<col/>
							<col/>
							<col span="2"/>
							<col/>
						</colgroup>
						<thead>
							<tr>
								<th align="left">S.No.</th>
								<th align="center">Name</th>
								<th align="center" colspan="2">Density (g·cm<sup>-3</sup>) </th>
								<th align="center">Porosity (&#x25;)</th>
							</tr>
						</thead>
						<tbody>
							<tr>
								<td align="left">7.</td>
								<td align="center" rowspan="2">ALR0</td>
								<td align="center">Theoretical </td>
								<td align="center">2.810</td>
								<td align="center" rowspan="2">1.067</td>
							</tr>
							<tr>
								<td align="left">8.</td>
								<td align="center">Experimental </td>
								<td align="center">2.780</td>
							</tr>
							<tr>
								<td align="left">9.</td>
								<td align="center" rowspan="2">ALR5</td>
								<td align="center">Theoretical</td>
								<td align="center">2.8325</td>
								<td align="center" rowspan="2">1.64</td>
							</tr>
							<tr>
								<td align="left">10.</td>
								<td align="center">Experimental</td>
								<td align="center">2.786</td>
							</tr>
							<tr>
								<td align="left">11.</td>
								<td align="center" rowspan="2">ALR10</td>
								<td align="center">Theoretical</td>
								<td align="center">2.855</td>
								<td align="center" rowspan="2">2.10</td>
							</tr>
							<tr>
								<td align="left">12.</td>
								<td align="center">Experimental</td>
								<td align="center">2.795</td>
							</tr>
							<tr>
								<td align="left" rowspan="2">13.</td>
								<td align="center" rowspan="2">ALR15</td>
								<td align="center">Theoretical</td>
								<td align="center">2.8775</td>
								<td align="center" rowspan="2">2.73</td>
							</tr>
							<tr>
								<td align="center">Experimental</td>
								<td align="center">2.799</td>
							</tr>
						</tbody>
					</table>
				</table-wrap>
			</sec>
			<sec id="sec3.2">
				<label>3.2.</label>
				<title>Microhardness and microstructure</title>
				<p>The microstructure optic of the composite is used taking into account the quality and an assessment of the efficiency of the technology used by the composite. <xref ref-type="fig" rid="f2">Figure 2</xref> and <xref ref-type="fig" rid="f3">Fig. 3</xref> show the photomicrographs and the corresponding microhardness of the composite. From the images of the light microscope, we can see that the reinforcements were evenly distributed in the matrix material and also clearly show the increased content of reinforcement in the composite material.</p>
				<fig id="f2">
					<label>Figure 2</label>
					<caption>
						<title>Microstructure images of (a) ALR0, (b) ALR5, (c) ALR10 and (d) ALR15.</title>
					</caption>
					<graphic id="gra-2" xlink:href="REVMET-57-01-e185-gf2.png"/>
				</fig>
				<fig id="f3">
					<label>Figure 3</label>
					<caption>
						<title>Microhardness images of (a) ALR0, (b) ALR5, (c) ALR10 and (d) ALR15.</title>
					</caption>
					<graphic id="gra-3" xlink:href="REVMET-57-01-e185-gf3.png"/>
				</fig>
				<p>The effect of Redmud on the microhardness of the composite materials obtained from the hardness test. The hardness measurements are carried out on a Vickers microhardness testing machine. From the microhardness test, it has been observed that the hardness of the Al7075 + Redmud metal matrix composite increases with the addition of Redmud. It was higher than that of the base alloy Al 7075. The hardness of all the metal matrix composites was significantly higher than that of the base alloy.</p>
				<p>
					<xref ref-type="table" rid="t5">Table 5</xref> shows that the hardness measurement of metal matrix composites reinforced with Redmud in 5 times. From the measurement of the 5 times, the average is taken as a hardness of the metal matrix composite reinforced with red mud.</p>
				<table-wrap id="t5">
					<label>Table 5</label>
					<caption>
						<title>Hardness measurement of Redmud reinforced metal matrix composite in VHN</title>
					</caption>
					<table>
						<colgroup>
							<col/>
							<col/>
							<col/>
							<col/>
							<col/>
						</colgroup>
						<thead>
							<tr>
								<th align="left">Trails</th>
								<th align="left">ALR0</th>
								<th align="left">ALR5</th>
								<th align="left">ALR10</th>
								<th align="left">ALR15</th>
							</tr>
						</thead>
						<tbody>
							<tr>
								<td align="left">1st trail</td>
								<td align="left">142.5</td>
								<td align="left">175.0</td>
								<td align="left">179.3</td>
								<td align="left">183.6</td>
							</tr>
							<tr>
								<td align="left">2nd trail</td>
								<td align="left">134.1</td>
								<td align="left">176.5</td>
								<td align="left">181.0</td>
								<td align="left">179.8</td>
							</tr>
							<tr>
								<td align="left">3rd trail</td>
								<td align="left">140.7</td>
								<td align="left">173.2</td>
								<td align="left">176.3</td>
								<td align="left">180.1</td>
							</tr>
							<tr>
								<td align="left">4th trail</td>
								<td align="left">138.4</td>
								<td align="left">176.0</td>
								<td align="left">175.2</td>
								<td align="left">177.4</td>
							</tr>
							<tr>
								<td align="left">5th trail</td>
								<td align="left">136.1</td>
								<td align="left">177.1</td>
								<td align="left">181.6</td>
								<td align="left">185.0</td>
							</tr>
							<tr>
								<td align="left">Average</td>
								<td align="left">138.36</td>
								<td align="left">175.56</td>
								<td align="left">178.68</td>
								<td align="left">181.18</td>
							</tr>
						</tbody>
					</table>
				</table-wrap>
			</sec>
			<sec id="sec3.3">
				<label>3.3.</label>
				<title>Tensile strength</title>
				<p>Due to the low density of aluminium, the material is suitable for applications in the aerospace and automotive industries. The lower resistance of the aluminium alloy limits their applications. <xref ref-type="table" rid="t6">Table 6</xref> shows that the values obtained tensile strength values of Al 7075 metal matrix composites reinforced by redmud. The Al 7075 metal matrix composites reinforced with red mud show that the tensile strength increases compared to the base alloy. To increase the strength of the composite, the presence of hard reinforcing particles is used. The addition of Redmud particles mainly improves the impact on the rupture and the tensile strength of the composite material by transferring the stresses of the aluminium matrix (ductile) to the reinforced particles (brittle).</p>
				<table-wrap id="t6">
					<label>Table 6</label>
					<caption>
						<title>Tensile result for the Al7075/Redmud metal matrix composite</title>
					</caption>
					<table>
						<colgroup>
							<col/>
							<col/>
							<col/>
							<col/>
						</colgroup>
						<thead>
							<tr>
								<th align="left">Name</th>
								<th align="center">UTS in MPa</th>
								<th align="center">Peak Load in kN</th>
								<th align="center">Elongation in &#x25;</th>
							</tr>
						</thead>
						<tbody>
							<tr>
								<td align="left">ALR0</td>
								<td align="center">87</td>
								<td align="center">3.115</td>
								<td align="center">6.40</td>
							</tr>
							<tr>
								<td align="left">ALR5</td>
								<td align="center">326</td>
								<td align="center">11.720</td>
								<td align="center">12.0</td>
							</tr>
							<tr>
								<td align="left">ALR10</td>
								<td align="center">272</td>
								<td align="center">9.800</td>
								<td align="center">10.20</td>
							</tr>
							<tr>
								<td align="left">ALR15</td>
								<td align="center">223</td>
								<td align="center">8.040</td>
								<td align="center">10.0</td>
							</tr>
						</tbody>
					</table>
				</table-wrap>
				<p>The elongation of the metal matrix composite was also measured in the tensile test. The elongation in tension is the elongation that a material undergoes when it is pulled under tension. The ductility of the material is measured from the percentage of elongation. <xref ref-type="table" rid="t6">Table 6</xref> shows that the elongation values and peak load values of the metal matrix composites reinforced by Redmud. Here is the discussion on the peak load of the metal matrix composite, it is the maximum load that the test object can support during the test. The higher the tension required to create a certain stretch, the more rigid the material. </p>
			</sec>
			<sec id="sec3.4">
				<label>3.4.</label>
				<title>Fractography</title>
				<p>
					<xref ref-type="fig" rid="f4">Figure 4</xref> shows that the fracture surface of base Al 7075 and Al 7075 metal matrix composites. In this study of fractography from the aluminium composites, with the higher percentage of reinforcement used matrix cracks are adjacent to the Redmud particles and the limited amount of material flow is observed in the fractography. The following SEM images are in 1200x and 2500x magnifications and scale of 40 &#xb5;m and 20 &#xb5;m.</p>
				<fig id="f4">
					<label>Figure 4</label>
					<caption>
						<title>SEM micrographs of the tensile fracture surface of (a) ALR0, (b) ALR5, (c) ALR10 and (d) ALR15.</title>
					</caption>
					<graphic id="gra-4" xlink:href="REVMET-57-01-e185-gf4.png"/>
				</fig>
			</sec>
		</sec>
		<sec id="sec4">
			<label>4.</label>
			<title>Potentiodynamic polarization test</title>
			<p>Electrochemical behaviour of Al 7075 metal matrix composites in 3.5&#x25; NaCl solution at room temprature is shown in <xref ref-type="fig" rid="f5">Fig. 5</xref>. Corrosion current density and potential (Icorr &amp; Ecorr), betta cathodic (ßc), betta anodic (ßa) slopes and the corrosion rate are obtained from the cathodic and anodic region of the TAFEL scan and the results are tabulated in <xref ref-type="table" rid="t7">Table 7</xref>. In potentiodynamic polarization testing, values of potential started from -1.3 V and for all the metal matrix composites result for Ecorr values are in between the range of -700 mV to -800 mV, which is higher than base alloy Al 7075. </p>
			<fig id="f5">
				<label>Figure 5</label>
				<caption>
					<title>Polarization curve for: (a) ALR0, (b) ALR5, (c) ALR10 and (d) ALR15.</title>
				</caption>
				<graphic id="gra-5" xlink:href="REVMET-57-01-e185-gf5.png"/>
			</fig>
			<table-wrap id="t7">
				<label>Table 7</label>
				<caption>
					<title>Icorr, Ecorr and corrosion rate for Al 7075 metal matrix composites</title>
				</caption>
				<table>
					<colgroup>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
						<col/>
					</colgroup>
					<thead>
						<tr>
							<th align="left">Composition</th>
							<th align="center">ßa e-3V/decade</th>
							<th align="center">ßc e-3V/decade</th>
							<th align="center">Icorr &#xb5;A</th>
							<th align="center">Ecorr mV</th>
							<th align="center">Corrosion Rate mpy</th>
						</tr>
					</thead>
					<tbody>
						<tr>
							<td align="left">ALR0</td>
							<td align="center">148.5</td>
							<td align="center">596.9</td>
							<td align="center">8.590</td>
							<td align="center">-996.0</td>
							<td align="center">3.925</td>
						</tr>
						<tr>
							<td align="left">ALR5</td>
							<td align="center">42.00</td>
							<td align="center">763.9</td>
							<td align="center">5.910</td>
							<td align="center">-771.0</td>
							<td align="center">2.701</td>
						</tr>
						<tr>
							<td align="left">ALR10</td>
							<td align="center">41.10</td>
							<td align="center">405.0</td>
							<td align="center">4.970</td>
							<td align="center">-708.0</td>
							<td align="center">2.273</td>
						</tr>
						<tr>
							<td align="left">ALR15</td>
							<td align="center">40.20</td>
							<td align="center">540.9</td>
							<td align="center">3.270</td>
							<td align="center">-756.0</td>
							<td align="center">1.496</td>
						</tr>
					</tbody>
				</table>
			</table-wrap>
			<p>The corrosion current density (Icorr) values were decreased, while increasing the volume percentage of reinforcement (Redmud) particles. Naturally sand particles are corrodable, but here the addition of redmud into the Al 7075 alloy can increase the corrosion resistance by the physical properties of reinforcement.</p>
			<p>Increasing the volume percentage of reinforcement particle (redmud) increases the corrosion resistance of the Al 7075. Possibilities of corrosion is reducing due to the bonding between the reinforcement and matrix, while increasing the vol percentage of reinforcement. Uniform flow of reinforcement is the reason behind increasing the corrosion resistance. From <xref ref-type="table" rid="t7">Table 7</xref>, it has been found that the Al7075 composites show better corrosion resistance when compared with the base alloy Al7075.</p>
			<p>
				<xref ref-type="bibr" rid="B23">Shimizu <italic>et al.</italic> (1995)</xref> developed an Al7075/SiC metal matrix composite (MMC) using a squeeze casting process and investigated heat-treated MMC to increase the potential for pitting and resist stress corrosion cracking in NaCl solution at 3.5&#x25;.</p>
			<sec id="sec4.1">
				<label>4.1.</label>
				<title>SEM Analysis</title>
				<p>
					<xref ref-type="fig" rid="f6">Figure 6</xref> shows that the corrosion of Al 7075 base alloy and Al 7075 metal matrix composites in different volume percentages. 3.5&#x25; of NaCl solution is used for the potentiodynamic polarization testing process. NaCl is a highly corrosive medium for the both Al 7075 base alloy and Al 7075 metal matrix composites. Here, ALR5 composition is highly corroded when compare to the ALR15 composition. The reason behind the corrosion rate reduction is, Redmud was acting as a cathodic sites with the galvanic action.</p>
				<fig id="f6">
					<label>Figure 6</label>
					<caption>
						<title>SEM micrographs of the corroded: (a) ALR0, (b) ALR5, (c) ALR10 and (d) ALR15.</title>
					</caption>
					<graphic id="gra-6" xlink:href="REVMET-57-01-e185-gf6.png"/>
				</fig>
			</sec>
		</sec>
		<sec id="sec5" sec-type="conclusions">
			<label>5.</label>
			<title>Conclusions</title>
			<p>Testing results provided the following conclusions:</p>
			<list list-type="bullet">
				<list-item>
					<p>Experimental density of the fabricated composite was calculated by using Archimedes principle, which is higher than base matrix. </p>
				</list-item>
				<list-item>
					<p>Highest level of porosity for the fabricated composite is not exceeded 3&#x25;.</p>
				</list-item>
				<list-item>
					<p>The fabricated composite provide high hardness and tensile strength while compare to the base matrix.</p>
				</list-item>
				<list-item>
					<p>Microhardness of the composite was increased while increasing the reinforcement from 0&#x25; to 15&#x25;.</p>
				</list-item>
				<list-item>
					<p>Ultimate tensile strength of the composite is high at 5&#x25; of reinforcement addition, which is 326 MPa. It is higher than the base matrix.</p>
				</list-item>
				<list-item>
					<p>Elongation and Peak load both are more over same, increases up to 5&#x25; addition of reinforcement. Afterwards, slightly decreases.</p>
				</list-item>
				<list-item>
					<p>Al 7075 metal matrix composites provided lower corrosion rate than the base matrix in 3.5&#x25; NaCl solution. Increasing the volume percentage of redmud reduces the corrosion rate of the composites.</p>
				</list-item>
			</list>
		</sec>
	</body>
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