<?xml version="1.0" encoding="utf-8"?>
<XML>
<ISCJOURNAL>
<YEAR>2025</YEAR>
<VOL>5</VOL>
<NO>4</NO>
<PAGE_NO>9</PAGE_NO>
<ARTICLES>
			<ARTICLE>
				<TitleF></TitleF>
				<TitleE>Porosity-dependent mechanical properties of sintered titanium: RVE-based finite element modeling and Gibson–Ashby analysis</TitleE>
				<TitleLang_ID>en</TitleLang_ID>
				<ABSTRACTS>
					<ABSTRACT>
						<Language_ID>en</Language_ID>
						<CONTENT>Porous sintered titanium structures are widely used in biomedical and lightweight engineering applications due to their tunable mechanical performance and favorable biocompatibility. In this study, the porosity-dependent mechanical behavior of sintered titanium is investigated using a three-dimensional representative volume element (RVE) combined with finite element modeling. The RVE is constructed from an ordered arrangement of spherical titanium particles under periodicity, and sintering-induced neck growth is represented geometrically by controlled interparticle overlap achieved through systematic reduction of the RVE size. Uniaxial displacement-controlled loading is applied to extract the homogenized stress–strain response over a range of porosity levels. The simulations demonstrate a strong sensitivity of the effective elastic modulus, yield strength, and energy absorption capacity to relative density and neck evolution. The effective mechanical properties are evaluated through homogenization and analyzed within the framework of Gibson–Ashby scaling. The normalized stiffness, strength, and absorbed energy exhibit clear power-law relationships with relative density, with scaling exponents consistent with values reported for sintered and cellular metallic materials. The results highlight the critical role of microstructural architecture and particle connectivity in governing stiffness degradation, strength reduction, and energy absorption during densification. Overall, the proposed RVE-based numerical framework provides a physically consistent and computationally efficient tool for predicting the effective mechanical response of sintered titanium as a function of porosity, offering valuable insights for the design and optimization of porous titanium components in biomedical and structural applications.</CONTENT>
					</ABSTRACT>
				</ABSTRACTS>
				<PAGES>
					<PAGE>
						<FPAGE>323</FPAGE>
						<TPAGE>331</TPAGE>
					</PAGE>
				</PAGES>
				<AUTHORS>
					<AUTHOR>
						<NameE>Ata</NameE>
						<MidNameE></MidNameE>		
						<FamilyE>Khabaz-Aghdam</FamilyE>
						<Organizations>
							<Organization>Department of Aeronautical Engineering, Faculty of Aviation and Space Sciences</Organization>
						</Organizations>
						<Universities>
							<University>University of Kyrenia, Kyrenia, Mersin 10</University>
						</Universities>
						<Countries>
							<Country>Turkey</Country>
						</Countries>
						<EMAILS>
							<Email>ata.khabazaghdam@kyrenia.edu.tr</Email>			
						</EMAILS>
					</AUTHOR>
					<AUTHOR>
						<NameE>Takunda</NameE>
						<MidNameE></MidNameE>		
						<FamilyE>Happison Nyenyewa</FamilyE>
						<Organizations>
							<Organization>Department of Mechanical Engineering, Faculty of Engineering</Organization>
						</Organizations>
						<Universities>
							<University>University of Kyrenia, Mersin 10, Kyrenia</University>
						</Universities>
						<Countries>
							<Country>Turkey</Country>
						</Countries>
						<EMAILS>
							<Email></Email>			
						</EMAILS>
					</AUTHOR>
					<AUTHOR>
						<NameE>Jacob</NameE>
						<MidNameE></MidNameE>		
						<FamilyE>Kabole Kahungwa</FamilyE>
						<Organizations>
							<Organization>Department of Mechanical Engineering, Faculty of Engineering</Organization>
						</Organizations>
						<Universities>
							<University>University of Kyrenia, Mersin 10, Kyrenia</University>
						</Universities>
						<Countries>
							<Country>Turkey</Country>
						</Countries>
						<EMAILS>
							<Email></Email>			
						</EMAILS>
					</AUTHOR>
					<AUTHOR>
						<NameE>Cengiz</NameE>
						<MidNameE></MidNameE>		
						<FamilyE>Mesut Bükeç</FamilyE>
						<Organizations>
							<Organization>Department of Aviation Management, Faculty of Aviation and Space Sciences</Organization>
						</Organizations>
						<Universities>
							<University>University of Kyrenia, Kyrenia, Mersin 10</University>
						</Universities>
						<Countries>
							<Country>Turkey</Country>
						</Countries>
						<EMAILS>
							<Email></Email>			
						</EMAILS>
					</AUTHOR>
					<AUTHOR>
						<NameE>Halise</NameE>
						<MidNameE></MidNameE>		
						<FamilyE>Duygu Özalp</FamilyE>
						<Organizations>
							<Organization>Department of Sociology</Organization>
						</Organizations>
						<Universities>
							<University>Başkent University, Ankara</University>
						</Universities>
						<Countries>
							<Country>Turkey</Country>
						</Countries>
						<EMAILS>
							<Email></Email>			
						</EMAILS>
					</AUTHOR>
				</AUTHORS>
				<KEYWORDS>
					<KEYWORD>
						<KeyText>Sintered titanium</KeyText>
					</KEYWORD>
					<KEYWORD>
						<KeyText>Representative volume element (RVE)</KeyText>
					</KEYWORD>
					<KEYWORD>
						<KeyText>Finite element modeling (FEM)</KeyText>
					</KEYWORD>
					<KEYWORD>
						<KeyText>Mechanical properties</KeyText>
					</KEYWORD>
					<KEYWORD>
						<KeyText>Gibson–Ashby scaling laws</KeyText>
					</KEYWORD>
				</KEYWORDS>
				<PDFFileName>Vol 5 No 4 Paper 6.pdf</PDFFileName>
				<REFRENCES>
				<REFRENCE>
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				</REFRENCE>
					</REFRENCES>
			</ARTICLE>
			</ARTICLES>
</ISCJOURNAL>
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