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<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>CFD Simulation of the Aqueous Humour in Healthy or Glaucomatous Conditions</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>369</FirstPage>
			<LastPage>390</LastPage>
			<ELocationID EIdType="pii">106018</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.410638.1780</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>O. Anwar</FirstName>
					<LastName>Bég</LastName>
<Affiliation>Multi-Physical Engineering Sciences Group, Mechanical Engineering Department, Corrosion and Coatings Lab, Room 3-08, SEE Building, University of Salford, Manchester, M54WT, UK</Affiliation>

</Author>
<Author>
					<FirstName>U.I.</FirstName>
					<LastName>Usman</LastName>
<Affiliation>Simulation Engineer, Shell Petroleum, London, UK</Affiliation>

</Author>
<Author>
					<FirstName>Tasveer A.</FirstName>
					<LastName>Bég</LastName>
<Affiliation>Engineering Mechanics Research, Israfil House, Dickenson Rd., Manchester, M13, UK</Affiliation>

</Author>
<Author>
					<FirstName>M. M.</FirstName>
					<LastName>Channakote</LastName>
<Affiliation>Department of Mathematics and Statistics, M. S. Ramaiah University of Applied Sciences, Bengaluru, Karnataka, 560054, India</Affiliation>

</Author>
<Author>
					<FirstName>H. J.</FirstName>
					<LastName>Leonard</LastName>
<Affiliation>Multi-Physical Engineering Sciences Group, Mechanical Engineering Department, Corrosion and Coatings Lab, Room 3-08, SEE Building, University of Salford, Manchester, M54WT, UK</Affiliation>

</Author>
<Author>
					<FirstName>M.M.</FirstName>
					<LastName>Bhatti</LastName>

						<AffiliationInfo>
						<Affiliation>Department of Physics, College of Science, Korea University, 145 Anam-ro, Seongbuk-gu, Seoul 02841, Republic of Korea</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Material Science Innovation and Modelling (MaSIM) Research Focus Area, North-West University (Mafikeng Campus), Private Bag X2046, Mmabatho 2735, South Africa</Affiliation>
						</AffiliationInfo>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>02</Month>
					<Day>06</Day>
				</PubDate>
			</History>
		<Abstract>This article presents a computational fluid dynamics (CFD) simulation of aqueous humour flow within the anterior chamber of the eye, comparing healthy and glaucomatous conditions. A simplified 2-dimensional cross-sectional geometry was developed using ANSYS Fluent 2024 R2 Design Modeller, with the trabecular meshwork represented as a porous medium, accounting for its role in flow resistance. Viscous resistances of 2.43 x 1013 m-2 and 6.5 x 1013 m-2 for healthy and glaucomatous cases respectively, were derived from literature and applied to simulate variations in the outflow. A mesh independence study was included. In the healthy model, the simulation peak intraocular pressure of 15.08 mmHg was consistent with normal physiological limits. In the glaucomatous case, intraocular pressure increased to 40.45 mmHg, representing a 168% rise, also agreeing with existing literature. The visualisation of flow fields revealed similar inlet velocity profiles but notable differences in pressure gradients, streamline curvature and vorticity distribution near the trabecular meshwork in the glaucomatous configuration. These numerical trends are within ±5% of existing literature results and confirm the validity of the study. The anterior chamber’s fluid sensitivity is clearly highlighted in the results, confirming the role of CFD as a predictive tool for understanding ocular fluid mechanics and supporting diagnostic and surgical decision making in glaucoma management.</Abstract>
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			<Param Name="value">Ocular fluid dynamics</Param>
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			<Param Name="value">aqueous humour</Param>
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			<Param Name="value">anterior chamber</Param>
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			<Param Name="value">glaucomatous conditions</Param>
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			<Object Type="keyword">
			<Param Name="value">trabecular meshwork</Param>
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			<Object Type="keyword">
			<Param Name="value">Darcy porous medium</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Intraocular pressure</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">streamline curvature</Param>
			</Object>
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<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_106018_91f02c752a7ec1fb7560103f2944f021.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Influence of Spanwise FGM and Numerical Parameters on the Fluid-Structure Interaction Response of a Cantilevered Plate Wing</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>391</FirstPage>
			<LastPage>412</LastPage>
			<ELocationID EIdType="pii">106122</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.410596.1778</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Mohamed S</FirstName>
					<LastName>Alzahrani</LastName>
<Affiliation>Department of Mechanical Engineering, Faculty of Engineering, King Abdulaziz University, Jeddah, Saudi Arabia</Affiliation>

</Author>
<Author>
					<FirstName>Hassan</FirstName>
					<LastName>Qanash</LastName>
<Affiliation>Department of Mechanical Engineering, Faculty of Engineering, King Abdulaziz University, Jeddah, Saudi Arabia</Affiliation>

</Author>
<Author>
					<FirstName>Mohamed S</FirstName>
					<LastName>Abdelwaheed</LastName>
<Affiliation>Department of Mechanical Engineering, Faculty of Engineering, King Abdulaziz University, Jeddah, Saudi Arabia</Affiliation>

</Author>
<Author>
					<FirstName>Mohamed A</FirstName>
					<LastName>Elltaher</LastName>

						<AffiliationInfo>
						<Affiliation>Department of Mechanical Engineering, Faculty of Engineering, King Abdulaziz University, Jeddah, Saudi Arabia</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Department of Mechanical Design and Production, Faculty of Engineering, Zagazig University, Egypt</Affiliation>
						</AffiliationInfo>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>02</Month>
					<Day>05</Day>
				</PubDate>
			</History>
		<Abstract>This study investigates the nonlinear aeroelastic response and flutter behavior of a cantilevered plate wing using a two-way fluid–structure interaction framework in ANSYS, coupling Fluent and Mechanical. Both isotropic Aluminum and a spanwise functionally graded Al/Al₂O₃ material system are examined. The aerodynamic solver is validated against published S809 airfoil data, followed by validation of the cantilevered wing model. A sensitivity analysis is performed by varying the time step size (0.02–0.002 s) and the number of coupling iterations (5 and 10). Larger time steps introduce fluctuations in peak oscillation amplitudes and can delay growth through the critical flow speed window, whereas smaller time steps reduce these fluctuations and diminish iteration sensitivity. A mid-range configuration (∆t = 0.005 s, 10 iterations) provides results comparable to the finest settings at substantially lower computational cost. Using these parameters, the aeroelastic response of a spanwise functionally graded wing—constructed by dividing the span into ten segments with linear grading (k = 1)—is assessed. The FGM wing exhibits no flutter within the investigated flow speed range and shows markedly reduced tip displacement, maintaining RMS amplitudes below 0.01 mm, in contrast to the Aluminum baseline, which displays the expected increase in response with flow speed. The results demonstrate that a time step of 0.005 s with ten coupling iterations is sufficient for reliable flutter prediction under ANSYS student license constraints, and that spanwise FGM application significantly enhances aeroelastic stability.</Abstract>
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			<Object Type="keyword">
			<Param Name="value">Vibration and Instability</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Aeroelastic analysis</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Flutter prediction</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Fluid-Structure Interaction</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Functionally Graded Material</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nonlinear analysis</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Finite volume and CFD</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_106122_0a0cfdc951bd16447ee88774fd90c2bc.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Enhancing the Thermal Performance of Parabolic Trough Collectors Using Nano-Enhanced Absorber Coatings: A Comparative Study of Fe3O4, Al2O3 and Hybrid Fe3O4- Al2O3 Coatings</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>413</FirstPage>
			<LastPage>424</LastPage>
			<ELocationID EIdType="pii">106173</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.411481.1792</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Sathish</FirstName>
					<LastName>Thanikodi</LastName>
<Affiliation>Department of Mechanical Engineering, Saveetha School of Engineering, Saveetha Institute of Medical And Technical Sciences, Chennai, Tamil Nadu, Pin Code-602105, India</Affiliation>

</Author>
<Author>
					<FirstName>Jaloladdin</FirstName>
					<LastName>Rajabov</LastName>
<Affiliation>Department of Transport systems, Urgench State University named after Abu Rayhan Biruni, Urgench, 14, Kh.Alimdjan str, Urgench city, 220100, Uzbekistan</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>02</Month>
					<Day>19</Day>
				</PubDate>
			</History>
		<Abstract>Solar thermal systems use parabolic trough collectors (PTCs) to concentrate sunlight on an absorber tube to create heat for various applications. They are efficient but have optical losses, heat dissipation, and reduced performance owing to dust and high-emissivity coatings. Hence, nanomaterials can improve absorber coatings&#039; heat retention and energy efficiency. This research paper is an examination of the impact of nano-enhanced coating on PTC thermal characteristics. The various types of coating were a hybrid coating of Fe3O4-Al2O3 nano-enhanced coating, Fe3O4 nano-enhanced coating, Al2O3 nano-enhanced coating and black matte tested in their effects on energy and exergy efficiency, heat absorption, and fluid outlet temperature. It was found that the hybrid Fe3O4-Al2O3 coating recorded the highest of 81.5 ᵒC fluid outlet temperature, maximum of 3186.4 W heat absorption, thermal efficiency of 79.38% or exergy efficiency of 42.88%. Fe3O4 was selected because it has a high optical absorption, and Al2O3 was selected because it has a high thermal conductivity, which allows heat transfer to be efficient and losses to be reduced. The most ineffective one was black matte coating because the highest 59.4ᵒC fluid temperature and 42.57% thermal efficiency. Therefore, the nanomaterials enhance the power of PTC and this indicates that the materials have the possibility of maximizing the utilization of solar energy. The researchers established that solar thermal collector performance can be increased with the use of advanced nano-coatings, including the Fe3O4-Al2O3 hybrid and facilitation of the renewable, efficient, and sustainable renewable energy systems.</Abstract>
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			<Object Type="keyword">
			<Param Name="value">Sustainable</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">solar</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Energy</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Exergy</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Efficiency</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">nanoparticles</Param>
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<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_106173_b75a54a1db001b92f47b4707bb7f448c.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>A Spectrally Accurate Shifted Lucas Collocation Framework for Fractional Lanchester Combat Dynamics with Time-Dependent Variable Coefficients</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>425</FirstPage>
			<LastPage>442</LastPage>
			<ELocationID EIdType="pii">106519</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.412544.1799</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>M. H.</FirstName>
					<LastName>Salama</LastName>
<Affiliation>Department of Mathematics, Faculty of Science, Kafrelsheikh University, Kafrelsheikh 33516, Egypt</Affiliation>

</Author>
<Author>
					<FirstName>H. A.</FirstName>
					<LastName>Zedan</LastName>
<Affiliation>Department of Mathematics, Faculty of Science, Kafrelsheikh University, Kafrelsheikh 33516, Egypt</Affiliation>

</Author>
<Author>
					<FirstName>W. M.</FirstName>
					<LastName>Abd-Elhameed</LastName>
<Affiliation>Department of Mathematics, Faculty of Science, Cairo University, Giza 12613, Egypt</Affiliation>

</Author>
<Author>
					<FirstName>Y. H.</FirstName>
					<LastName>Youssri</LastName>

						<AffiliationInfo>
						<Affiliation>Department of Mathematics, Faculty of Science, Cairo University, Giza 12613, Egypt</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Faculty of Engineering, Egypt University of Informatics, Knowledge City, New Administrative Capital 19519, Egypt</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Associate Fellow (AFHEA) of the Higher Education Academy (Advance HE), UK</Affiliation>
						</AffiliationInfo>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>10</Day>
				</PubDate>
			</History>
		<Abstract>This paper is confined to developing a rigorous computational framework using the shifted Lucas polynomials for the numerical treatment of the generalized fractional-order Lanchester combat model characterized by time-dependent variable coefficients. The method uses an exact operational matrix for the Caputo derivative to handle the singular kernel, thereby eliminating the need for numerical quadrature. A global polynomial projection at shifted Chebyshev–Gauss–Lobatto nodes eliminates predictor–corrector errors and preserves high-order accuracy under memory effects. A rigorous analysis employing a generalized Gronwall inequality establishes well-posedness and derives sharp stability bounds via Mittag–Leffler functions. Numerical investigations validate enhanced stability and efficiency, especially for memory effects and heavy-tail decay, and error estimates indicate super-geometric convergence.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Fractional dynamical systems</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Spectral collocation</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Caputo derivative</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Operational matrix</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Coupled fractional ODEs</Param>
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			<Object Type="keyword">
			<Param Name="value">Mittag-Leffler stability</Param>
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			<Object Type="keyword">
			<Param Name="value">numerical methods</Param>
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<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_106519_544b2ce5ad8c5d2ffc8edbc09eace3bb.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Numerical Simulation and Visualization of Newtonian and Non-Newtonian Hemodynamics in a Stenotic Blood Vessel</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>443</FirstPage>
			<LastPage>472</LastPage>
			<ELocationID EIdType="pii">106558</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.411829.1797</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Taiba</FirstName>
					<LastName>Hussain</LastName>
<Affiliation>MPESG, Corrosion Lab, 3-08, Aeronautical and Mechanical Engineering Division, University of Salford, M5 4WT, UK</Affiliation>

</Author>
<Author>
					<FirstName>O. Anwar</FirstName>
					<LastName>Bég</LastName>
<Affiliation>MPESG, Corrosion Lab, 3-08, Aeronautical and Mechanical Engineering Division, University of Salford, M5 4WT, UK</Affiliation>

</Author>
<Author>
					<FirstName>Sireetorn</FirstName>
					<LastName>Kuharat</LastName>
<Affiliation>MPESG, Corrosion Lab, 3-08, Aeronautical and Mechanical Engineering Division, University of Salford, M5 4WT, UK</Affiliation>

</Author>
<Author>
					<FirstName>Tasveer Anwar</FirstName>
					<LastName>Bég</LastName>
<Affiliation>Engineering Mechanics Research, Israfil House, Dickenson Rd., Manchester, M13, UK</Affiliation>

</Author>
<Author>
					<FirstName>M.M.</FirstName>
					<LastName>Bhatti</LastName>

						<AffiliationInfo>
						<Affiliation>Department of Physics, College of Science, Korea University, 145 Anam-ro, Seongbuk-gu, Seoul 02841, Republic of Korea</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Material Science Innovation and Modelling (MaSIM) Research Focus Area, North-West University (Mafikeng Campus), Private Bag X2046, Mmabatho 2735, South Africa</Affiliation>
						</AffiliationInfo>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>08</Day>
				</PubDate>
			</History>
		<Abstract>Cardiovascular disease (CVD) remains the leading cause of mortality worldwide, with atherosclerosis-driven stenoses significantly altering haemodynamic and influencing potential nanoparticle drug delivery outcomes. This study applies computational fluid dynamics (CFD) via ANSYS FLUENT finite volume software, to two-dimensional stenosed arteries of varying severities (30%, 50%, 70%) and shoulder lengths (2, 4, 6 mm). Two regimes have been compared: a steady Newtonian baseline, where viscosity and velocity remain constant and a physiologically realistic pulsatile non-Newtonian Carreau regime incorporating shear-thinning viscosity and cardiac-cycle effects. In the steady Newtonian simulations, velocity plots showed that increasing stenosis severity amplified throat jet velocities and extended recirculation zones, while shoulder length governed the sharpness and spatial extent of disturbed flow. The pulsatile Carreau model revealed systolic acceleration and diastolic deceleration in velocity contour plots, greater pressure drops with stenosis severity. It also showed wall shear stress (WSS) distributions characterised by high shear at stenotic throats and low or oscillatory shear effects downstream. These disturbed, low-WSS regions were identified as potential nanoparticle deposition sites for pharmacodynamics treatments, aligning with prior findings on plaque-prone haemodynamics. The results demonstrate that stenosis severity amplifies haemodynamic disturbances, while shoulder length shapes their distribution, together influencing the likelihood of nanoparticle residence and deposition. These findings are consistent with published literature, supporting CFD as a predictive tool for assessing hemodynamics. Future research could integrate deformable arterial walls through fluid–structure interaction (FSI), patient-specific geometries, and explicit nanoparticle transport for drug delivery in clinical translation.</Abstract>
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			<Object Type="keyword">
			<Param Name="value">Hemodynamics</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">ANSYS FLUENT, atherosclerosis-driven stenoses, shoulder length shapes, cardiac-cycle effects, throat jet velocities, recirculation zones, wall shear stress (WSS)</Param>
			</Object>
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<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_106558_f9aa4d16280e930d06b36094b53ecdfc.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Dynamic Response and Damping of Viscoelastic Microtubules: Effects of N_S Configurations and Cytosolic Environments</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>473</FirstPage>
			<LastPage>496</LastPage>
			<ELocationID EIdType="pii">106559</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.409178.1758</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Ali</FirstName>
					<LastName>Giv</LastName>
<Affiliation>Department of Solid Mechanics, Faculty of Mechanical Engineering, University of Kashan, Kashan, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Ali</FirstName>
					<LastName>Ghorbanpour Arani</LastName>
<Affiliation>Department of Solid Mechanics, Faculty of Mechanical Engineering, University of Kashan, Kashan, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Elham</FirstName>
					<LastName>Haghparast</LastName>
<Affiliation>MD student, Medical School. Medical university of Kashan, Kashan</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>This study investigates the vibrational behavior of anisotropic microtubules (MTs) immersed in the viscous cytosolic fluid using both classical and higher-order beam theories (HOBTs). For the first time, multiple N_S configurations of MTs, along with their precise geometrical characteristics, are analyzed within a novel unified vibration–mechanics framework. The nonlocal strain gradient theory (NSGT) is employed to incorporate size-dependent effects, while surface elasticity theory ensures nanoscale accuracy. Viscoelastic models are integrated for both MTs and their surrounding medium.&lt;br /&gt;The intrinsic structural damping of microtubules is examined via the Kelvin–Voigt viscoelastic damping coefficient (retardation time), and the influence of the cytosolic viscous fluid damping on both natural frequencies and damping ratios is thoroughly analyzed. Additional parameters such as the nonlocal parameter, material length scale parameter, microtubule length and various beam theory are also systematically explored. The governing equations and boundary conditions are derived from Hamilton’s principle and numerically solved using the Differential Quadrature (DQ) method, enhanced with a CBCGE scheme for efficient boundary implementation.&lt;br /&gt;Results reveal that increasing either the structural damping of the MTs or the cytosolic fluid viscosity leads to greater overall damping and a reduction in natural frequencies. A critical retardation time is identified, beyond which the damping ratio rapidly increases, the natural frequencies sharply drop, and the system transitions to a non-oscillatory state. The magnitude of this critical time aligns well with previously reported nanoscale retardation times. &lt;br /&gt;The same trend is also observed across different N_S configurations, indicating that smaller microtubules tend to possess higher natural frequencies. These findings highlight the importance of viscoelastic behavior—particularly retardation effects—in understanding cellular mechanics, cancer treatment, disease diagnosis, and bio-nanotechnology advancements.</Abstract>
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			<Object Type="keyword">
			<Param Name="value">Kelvin–Voigt viscoelastic</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Retardation time</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Viscoelastic bio-medium</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Anisotropic protein microtubules</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Higher-order beam theories</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nonlocal strain gradient theory</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Surface elasticity</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_106559_e9c248800c2969ec20b64f101705a62a.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Void Effects on Plane Wave Propagation in a Nonlocal Microstretch Thermoelastic Medium with Initial Stress and Magnetic Field under Three Phase Lag Theory</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>497</FirstPage>
			<LastPage>513</LastPage>
			<ELocationID EIdType="pii">107346</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.412854.1806</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Ambreen</FirstName>
					<LastName>A. Khan</LastName>
<Affiliation>Department of Mathematics and Statistics, International Islamic University, Islamabad, Pakistan</Affiliation>

</Author>
<Author>
					<FirstName>Noor</FirstName>
					<LastName>Zoha</LastName>
<Affiliation>Department of Mathematics and Statistics, International Islamic University, Islamabad, Pakistan</Affiliation>

</Author>
<Author>
					<FirstName>R</FirstName>
					<LastName>Ellahi</LastName>

						<AffiliationInfo>
						<Affiliation>Department of Mathematics and Statistics, International Islamic University, Islamabad, Pakistan</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Center for Modeling &amp; Computer Simulation, Research Institute, King Fahd University of Petroleum &amp; Minerals, Dhahran, Saudi Arabia</Affiliation>
						</AffiliationInfo>

</Author>
<Author>
					<FirstName>Sadiq M.</FirstName>
					<LastName>Sait</LastName>

						<AffiliationInfo>
						<Affiliation>Center for Communications and IT Research, Research Institute, King Fahd University of Petroleum &amp; Minerals, Dhahran-31261, Saudi Arabia</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Interdisciplinary Research Center for Smart Mobility and Logistics, King Fahd University of Petroleum &amp; Minerals, Dhahran, Saudi Arabia</Affiliation>
						</AffiliationInfo>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>16</Day>
				</PubDate>
			</History>
		<Abstract>In this paper, the reflection of plane waves at a free surface of a nonlocal microstretch thermoelastic medium is investigated within the framework of the three-phase-lag (TPL) heat conduction theory. The model incorporates the combined effects of nonlocal elasticity, voids, magnetic field, and initial stress. The governing equations are formulated and solved to obtain analytical expressions for the amplitude ratios and energy ratios of reflected longitudinal and coupled transverse waves propagating with distinct phase velocities. Numerical computations are performed to examine the graphical influence of key physical parameters on wave characteristics. The results indicate that the void parameter generally reduces the amplitude ratios, whereas the nonlocal parameter significantly influences transverse wave components. The magnetic field predominantly affects longitudinal wave reflection, while initial stress produces contrasting variations in amplitude ratios. It is further observed that transverse wave amplitudes vanish at limiting angles of incidence, and the primary longitudinal wave remains dominant. Energy analysis confirms that the sum of energy ratios is unity for all angles of incidence, ensuring conservation of energy. The present study provides useful insights into wave propagation phenomena in complex thermoelastic materials with microstructural effects and external fields.</Abstract>
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			<Object Type="keyword">
			<Param Name="value">Void parameter</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">magnetic field</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Initial stress</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Energy Ratio</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Wave reflection</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Thermoelasticity</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Microstretch medium</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Three-phase-lag theory</Param>
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		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_107346_379102d2b3f050c53235e61e63ac2b7a.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>The intricate link between anterior cruciate ligament rupture and lower limb muscle fatigue: Musculoskeletal Modeling</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>514</FirstPage>
			<LastPage>525</LastPage>
			<ELocationID EIdType="pii">107347</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.409534.1765</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Zeynab</FirstName>
					<LastName>Saghaeinooshabadi</LastName>
<Affiliation>School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mohammad Reza</FirstName>
					<LastName>Zakerzadeh</LastName>
<Affiliation>School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Moahammad Ali</FirstName>
					<LastName>Nazari</LastName>

						<AffiliationInfo>
						<Affiliation>School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Université Grenoble Alpes, CNRS, Grenoble INP, TIMC, Grenoble, France</Affiliation>
						</AffiliationInfo>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>01</Month>
					<Day>06</Day>
				</PubDate>
			</History>
		<Abstract>Objective Anterior Cruciate Ligament (ACL) rupture can independently affect an individual’s quality of life. This impact becomes more significant when fatigue and intense activity are involved. The aim of this study is to investigate the muscle forces generated in various muscles of the healthy and injured leg using musculoskeletal modeling in OpenSim software.&lt;br /&gt;Methods In this study, a participant with unilateral ACL rupture was asked to perform a one-hour walking protocol. Kinematic data were recorded using reflective markers and motion capture cameras, while kinetic data were collected via force plates. These data were used to model the gait and calculate muscle forces in different leg muscles using full inverse analysis workflow.&lt;br /&gt;Results Notable differences were observed in muscle forces between the healthy and injured legs. These differences were particularly evident in the Semimembranosus, Soleus and Gracilis muscles. The Vastus Medialis and Vastus Intermedius of the injured leg produced up to 30% more force compared to the corresponding muscles in the healthy leg during the gait cycle, while the Soleus muscle in the healthy leg generated 47% to 74% greater force Relative to the contralateral limb. The Gracilis muscle also showed more than 45% difference in force production favoring the injured leg.&lt;br /&gt;Conclusion Dynamic musculoskeletal modeling was used as a more comprehensive method than surface electromyography for assessing different muscles even deep muscles in patients with musculoskeletal disorders. The results agree with EMG study for Vastus Medialis, Gastrocnemius Lateralis and Soleus. Gastrocnemius Medialis showed an approximate agreement with IEMG (Integrated Electro MyoGraphy) results. The behavior of the other surface muscles does not comply with IEMG results. This shows that a better modeling which includes the ligaments is needed.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Musculoskeletal modeling</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Anterior cruciate ligament injury</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">OpenSim</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">muscle fatigue</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Inverse kinematics and dynamics</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Gait Analysis</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Computed muscle control</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_107347_e580b303d24f570b602db2e073abde5e.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>A Laplace Transform Approach for Static Analysis of Cracked Axially Functionally Graded Beams with Variable Cross Section</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>526</FirstPage>
			<LastPage>537</LastPage>
			<ELocationID EIdType="pii">107460</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.415461.1837</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Şeref Doğuşcan</FirstName>
					<LastName>Akbaş</LastName>
<Affiliation>Department of Civil Engineering, Bursa Technical University, Mimar Sinan Campus, Bursa, 16310, Turkey</Affiliation>
<Identifier Source="ORCID">0000-0001-5327-3406</Identifier>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>05</Month>
					<Day>29</Day>
				</PubDate>
			</History>
		<Abstract>This study presents a comprehensive analytical investigation of the static analysis of a cracked axially functionally graded cantilever beam with exponentially varying material properties and cross-sectional geometry in the longitudinal direction. The crack is defined in the system using an equivalent rotational spring model. The main focus of this study is to solve this system, which contains complex discontinuities and variable coefficient differential equations, within a high-precision analytical framework, eliminating the computational cost imposed by numerical methods. Laplace transform method is effectively applied in solving the governing equations. The developed analytical model can express the effect of material gradient and crack stiffness parameters on beam deflection in closed form. The obtained analytical results are compared with exact integration solutions in the literature under different crack stiffness values. This study provides a faster, mathematically stable, and reliable solution method for functionally graded structures compared to traditional numerical methods, thus creating a unique and powerful analytical infrastructure for structural health monitoring and design optimization processes.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Functionally Graded Materials</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Cracked Beam</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Variable Cross-Section Beam</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Static Analysis, Laplace Transform</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_107460_c70cd89164170efcb593a116b7e6a295.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>University of Tehran Press</PublisherName>
				<JournalTitle>Journal of Computational Applied Mechanics</JournalTitle>
				<Issn>2423-6713</Issn>
				<Volume>57</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Double-Diffusive Heat and Mass Transfer in Unsteady MHD Casson Nanofluid Flow over a Bidirectional Stretching Surface with Cattaneo–Christov Heat Flux</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>538</FirstPage>
			<LastPage>553</LastPage>
			<ELocationID EIdType="pii">107520</ELocationID>
			
<ELocationID EIdType="doi">10.22059/jcamech.2026.416706.1852</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Ji-Huan</FirstName>
					<LastName>He</LastName>
<Affiliation>School of Information Engineering, Yango University, Fuzhou, China</Affiliation>

</Author>
<Author>
					<FirstName>M. Y</FirstName>
					<LastName>Adamu</LastName>
<Affiliation>Abubakar Tafawa Balewa University, Bauchi, Nigeria</Affiliation>

</Author>
<Author>
					<FirstName>Isah</FirstName>
					<LastName>Abdullahi</LastName>

						<AffiliationInfo>
						<Affiliation>School of Information Engineering, Yango University, Fuzhou, China</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Abubakar Tafawa Balewa University, Bauchi, Nigeria</Affiliation>
						</AffiliationInfo>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>06</Month>
					<Day>19</Day>
				</PubDate>
			</History>
		<Abstract>This work presents a theoretical investigation on unsteady magnetohydrodynamic (MHD) boundary layer flow of Casson nanofluids over a bidirectional stretching surface, with an emphasis on double-diffusive heat and mass transfer. To overcome the limitation of classical Fourier’s law, the Cattaneo–Christov heat flux model is employed to consider thermal relaxation time and finite heat propagation velocity. The mathematical model fully couples multiple physical mechanisms including thermal radiation, viscous dissipation, porous medium effect, Brownian motion and thermophoresis. Based on similarity transformations, the partial differential equations governing mass, momentum, energy and concentration are converted into a set of coupled ordinary differential equations. The calculated results are proven to be reliable through comparison with previous research outcomes. We systematically discuss the effects of various dimensionless parameters on flow field, temperature field and nanoparticle concentration field. It is observed that magnetic field, porosity and unsteadiness suppress flow velocity, while a larger Casson parameter enhances fluid movement. Temperature distribution is elevated by thermal radiation, viscous dissipation, Brownian motion and thermophoresis, and reduced by thermal relaxation. Concentration decreases with increasing Schmidt number and Brownian motion parameter, but increases with the rise of thermophoresis parameter. Furthermore, the growth of thermophoresis leads to a reduction in skin friction coefficient, local Nusselt number and local Sherwood number. This research deepens the understanding of multi-physical coupled transport in non-Newtonian nanofluids, and the results have broad application prospects in biomedical equipment, polymer production, heat exchangers and energy engineering.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">double diffusion</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">heat and mass transfer</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">MHD flow</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Casson nanofluid</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Cattaneo–Christov heat flux</Param>
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			<Object Type="keyword">
			<Param Name="value">bidirectional stretching surface</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">thermal radiation</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">viscous dissipation</Param>
			</Object>
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<ArchiveCopySource DocType="pdf">https://jcamech.ut.ac.ir/article_107520_9acb56599a56cd4a099761c4b9c94173.pdf</ArchiveCopySource>
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