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<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Experimental Investigation of Residual Stress Measurement on Cold Roll Bonded Al/Cu Composite by Incremental Hole-Drilling Method</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>1</FirstPage>
			<LastPage>11</LastPage>
			<ELocationID EIdType="pii">9657</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.34303.1682</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Amirmasood</FirstName>
					<LastName>Rahimijonoush</LastName>
<Affiliation>Faculty of Mechanical Engineering, University of Kashan, 8731753153, Kashan, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mohammad</FirstName>
					<LastName>Honarpisheh</LastName>
<Affiliation>Faculty of Mechanical Engineering, University of Kashan, 8731753153, Kashan, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Amir</FirstName>
					<LastName>Abdollahi</LastName>
<Affiliation>Faculty of Mechanical Engineering, University of Kashan, 8731753153, Kashan, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mehdi</FirstName>
					<LastName>Mohammadimehr</LastName>
<Affiliation>Faculty of Mechanical Engineering, University of Kashan, 8731753153, Kashan, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>05</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>Hole drilling is a semi-destructive procedure used to measure residual stress. This type of stress, caused by mechanical and thermal effects, can significantly impact the lifetime of composite specimens. This paper studies the residual stress measurement on aluminum-copper composite specimens. The experimental procedure involved creating five different composite specimens using a rolling machine, and then using ABAQUS software in FEA analysis to calculate the calibration coefficients. The American standard ASTM E837 was used to determine the residual stress measurement. The specimens are manufactured through the Cold Roll Bonding (CRB) process with a rolling machine. The incremental hole-drilling strain gauge method was used, with the MTS-3000 Restan machine, to measure the residual stresses. The aluminum-copper composite specimens were manufactured in different sequences. The results showed that the ultimate tensile strength of aluminum mono-layer was lower than all composite specimens. On the other hand, the ultimate tensile strength of the copper mono-layer was higher than all samples, except rolled Cu-Cu one. Furthermore, a comparison between two-layer and three-layer composite specimens showed that the two-layer specimen stored more residual stress. In general, copper metal has stored more residual stress than aluminum metal.</Abstract>
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			<Object Type="keyword">
			<Param Name="value">Residual Stress</Param>
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			<Object Type="keyword">
			<Param Name="value">Al/Cu Composite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Cold Roll Bonding</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Incremental Hole-Drilling</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Mechanical properties</Param>
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<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9657_857f2af68208140cfa6046ba870be058.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Performance Evaluation of Epoxy-Based Natural Composites Reinforced with Flax and Flax-Ramie Fiber</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>13</FirstPage>
			<LastPage>22</LastPage>
			<ELocationID EIdType="pii">9660</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.35217.1723</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Nidhi</FirstName>
					<LastName>Bangalore Chandrashekar</LastName>
<Affiliation>Department of Mechanical Engineering, RV College of Engineering, Bengaluru, 560059, India</Affiliation>

</Author>
<Author>
					<FirstName>Ramesh Suryanarayana</FirstName>
					<LastName>Sharma</LastName>
<Affiliation>Department of Mechanical Engineering, RV College of Engineering, Bengaluru, 560059, India</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>09</Month>
					<Day>04</Day>
				</PubDate>
			</History>
		<Abstract>Growing environmental concerns and regulatory pressure have necessitated the requirement for natural fiber-based composites for various applications. . This paper focuses on the performance evaluation of epoxy reinforced with Flax and flax-ramie fiber hybrid composites. The laminates were developed through the hand layup technique with Flax and Ramie fibers using epoxy resin. The prepared samples were further analyzed under various dynamic and static conditions, including Fast Fourier Transform (FFT) analysis, impact testing, water absorption testing, and density measurement. The flax-ramie hybrid composite shows dynamic and static properties, including better vibration control, impact resistance, and lower moisture absorption, compared to the flax fiber composite. With a density of 1.17 g/cm³, the absorbs more energy (10.47 J) and withstands higher impact forces (2.08 N). These characteristics make the hybrid composite more suitable for impact-prone and water-sensitive applications.
 
 
 
 
 
 
 </Abstract>
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			<Param Name="value">Flax Fiber</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Ramie Fiber</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Natural fiber composite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Fast Fourier Transform</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Impact analysis</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9660_e8054dd75bfbaddf273dc35d58aeedef.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Mechanical Testing of Novel and Conventional Geopolymer Brick Dried under Passive Solar Dryer with Ferric Chloride Dihydrate as Phase Change Material</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>23</FirstPage>
			<LastPage>35</LastPage>
			<ELocationID EIdType="pii">9798</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.34977.1712</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Ashok Kumar Jeevan</FirstName>
					<LastName>Jeevan</LastName>
<Affiliation>Department of Mechanical Engineering, Kalasalingam University, Krishnan Koil, Virudhunagar District, 626126, India</Affiliation>

</Author>
<Author>
					<FirstName>Muthuvel</FirstName>
					<LastName>Sattanathan</LastName>
<Affiliation>Department of Mechanical Engineering, Kalasalingam University, Krishnan Koil, Virudhunagar District, 626126, India</Affiliation>

</Author>
<Author>
					<FirstName>Sudhakara Pandian</FirstName>
					<LastName>Ranjitharamasamy</LastName>
<Affiliation>Vellore Institute of Technology, School of Mechanical Engineering, Vellore, 632014, India</Affiliation>

</Author>
<Author>
					<FirstName>Gopinath</FirstName>
					<LastName>Govindan Radhakrishnan</LastName>
<Affiliation>M. Kumarasamy College of Engineering, Karur, India</Affiliation>

</Author>
<Author>
					<FirstName>Rajesh Kanna</FirstName>
					<LastName>Govindhan Radhakrishnan</LastName>
<Affiliation>High Energy Batteries (India) Limited, Pudukottai, 622515, India</Affiliation>

</Author>
<Author>
					<FirstName>Rajendra Prasad</FirstName>
					<LastName>Arani</LastName>
<Affiliation>Sri Sai Ram Engineering College, West Tambaram, Chennai, 600044, India</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>08</Month>
					<Day>10</Day>
				</PubDate>
			</History>
		<Abstract>Conventionally, in Geopolymer bricks (GPB), fly ash from power plants and ground granulated blast furnace slag are converted into bricks by chemical treatment. In this work, a novel GPB has been obtained by adding nano silica and rice husk ash to the conventional ingredients of GPB, along with Ferric Chloride Dihydrate, which is used as a phase change material to accelerate the curing time by utilizing its latent heat stored in the form of phase change. This novelty aims at introducing solar dryers with phase change materials in the areas of curing GPB, which have shown competent properties when compared to conventional bricks in the construction sector. It has been experimentally found that the solar drying method with Ferric Chloride Dihydrate (22 hours) utilizes a shorter curing time when compared to an electrical oven (24 hours) and open sun drying (24 hours). The properties of novel GPBs are evaluated by mechanical testing and compared with conventional GPBs. It has been experimentally observed that novel GPB exhibits higher compressive strength of 45 MPa, tensile strength of 4.5 MPa, and flexural strength of 6.5 MPa when compared to compressive strength of 41.5 MPa, tensile strength of 3.35 MPa, and flexural strength of 6.2 MPa as that of conventional GPB. Also in this study, Scanning Electron Microscopy (SEM) images of the damaged surfaces and energy-dispersive X-ray spectroscopy (EDX) analysis of novel GPB obtained from test results have been furnished. Smart quantitative results from EDX analysis show that the Oxygen Potassium content has the highest weight percentage and atomic percentage.</Abstract>
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			<Param Name="value">Geopolymer bricks (GPB)</Param>
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			<Object Type="keyword">
			<Param Name="value">Phase change material</Param>
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			<Object Type="keyword">
			<Param Name="value">Rice husk ash</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nano silica</Param>
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			<Object Type="keyword">
			<Param Name="value">Scanning electron microscopy</Param>
			</Object>
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<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9798_091d5a7d85872b96697164769e6e6989.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Study on Thermal, Mechanical and Dynamic Properties of Epoxy Matrix with Hybrid of ‎Nanoclay/Carbon Nanotube</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>37</FirstPage>
			<LastPage>56</LastPage>
			<ELocationID EIdType="pii">9598</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.34769.1698</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Shadi</FirstName>
					<LastName>Afshin</LastName>
<Affiliation>Mechanical Engineering Department, Razi University,  Kermanshah, 6714414971, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mohammad Hossein</FirstName>
					<LastName>Yas</LastName>
<Affiliation>Mechanical Engineering Department, Razi University,  Kermanshah, 6714414971, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>07</Month>
					<Day>16</Day>
				</PubDate>
			</History>
		<Abstract>Hybrid polymer nanocomposites (HPNCs) represent a promising class of materials for various engineering applications. This study investigates the impact of combining nano clay (NC) and carbon nanotubes (CNTs) on the thermal and mechanical properties of epoxy matrices. Mechanical and thermal properties of HPNCs were characterized using TGA, DMTA, TMA, and SEM, and tested for flexural, tensile, shear, hot plate, and modal analyses. The obtained results were compared with similar theoretical ones from the Halpin-Tsai method. Results indicate that incorporating up to 5 wt % of NC alongside epoxy/CNT nanocomposites enhances CNT dispersion, leading to improvements in degradation temperature (+1%), glass transition temperature (+10%), thermal stability (50% increase in residual ash), storage modulus in the plastic range (+39%), transverse bond density (+41%), thermal expansion coefficient (-17%), flexural strength (+17%), elastic modulus (+85%), shear modulus (+11%), and natural frequency of the beam (+42%).</Abstract>
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			<Object Type="keyword">
			<Param Name="value">hybrid nanocomposite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nanoclay</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Carbon nanotube</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Thermal and mechanical properties</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Halpin-Tsai</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9598_57b570b1bd14268e718bbb83056782ec.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Elaboration and Characterization of Waste Inked Paper-Poly (Vinyl Chloride) Composites: Effect of Paper Deinking</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>57</FirstPage>
			<LastPage>68</LastPage>
			<ELocationID EIdType="pii">9666</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.35931.1761</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Samira</FirstName>
					<LastName>Sahi</LastName>
<Affiliation>University of Bejaia, Faculty of Technology, Advanced Polymer Materials Laboratory, 06000, Bejaia, Algeria</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>11</Month>
					<Day>14</Day>
				</PubDate>
			</History>
		<Abstract>The waste paper poses environmental problems because it is a wood-based resource. Recovering it as fiber for the preparation of low-cost and environmentally-friendly composite materials offers significant environmental benefits, including reducing deforestation and the preservation of fossil resources. Our study presents an innovative approach by using waste inked and deinked paper as a reinforcement in thermoplastic polymer. Polyvinyl chloride (PVC)-based composites reinforced with waste inked paper (WIP) and waste de-inked paper (WDIP) fibers with loading rates ranging from 10% to 30% (Wt.%) were prepared. The effect of paper deinking processes on the mechanical, morphological, and physicochemical properties of the resulting composites was studied. Fourier Transform Infrared Spectroscopy (FTIR) analysis revealed the de-inking of paper after alkali-treatment. This result was confirmed by morphological analysis using optical spectroscopy. The results for the PVC/WIP and PVC/WDIP composites showed an improvement in the mechanical properties after the de-inking of the paper fiber. The tensile strength and the Young&#039;s modulus were increased by 16.90% and 37.80%, respectively, when 30% (Wt.%) of WDIP was added to PVC compared to WIP fiber. These results were confirmed by the optical spectroscopy (OS) analysis, where a better surface was observed in the PVC/WDIP composites. The water uptake test showed that the introduction of WDIP in PVC reduced water absorption by 18.38% compared with WIP fiber at a load charge of 30% (Wt.%). However, an increase in density was recorded. These results demonstrate that the incorporation of WDIP into PVC is not only feasible but also beneficial to environmental sustainability and economic growth.</Abstract>
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			<Param Name="value">Composite materials</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Polyvinyl chloride</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Waste paper</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Alkali-treatment</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">De-inking</Param>
			</Object>
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</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Modeling and Experimental Validation of Carbon Fiber-Kevlar Honeycomb Core Sandwich Structure</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>69</FirstPage>
			<LastPage>82</LastPage>
			<ELocationID EIdType="pii">9796</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.36296.1782</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Anil</FirstName>
					<LastName>Kumar</LastName>
<Affiliation>G. B. Pant DSEU Okhla-I Campus, New Delhi,110020, India</Affiliation>

</Author>
<Author>
					<FirstName>Sapna</FirstName>
					<LastName>Raghav</LastName>
<Affiliation>G. B. Pant DSEU Okhla-I Campus, New Delhi,110020, India</Affiliation>

</Author>
<Author>
					<FirstName>Jayant Pandurang</FirstName>
					<LastName>Supale</LastName>
<Affiliation>G. B. Pant DSEU Okhla-I Campus, New Delhi,110020, India</Affiliation>

</Author>
<Author>
					<FirstName>Gajanan Shravan</FirstName>
					<LastName>Datar</LastName>
<Affiliation>Government College of Engineering and Research, Avasari, Pune- 412406, India</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>12</Month>
					<Day>18</Day>
				</PubDate>
			</History>
		<Abstract>Composite sandwich structures are becoming more and more popular in the sports, automotive, and aerospace sectors because of their excellent strength-to-weight ratio. However, more research is required to fully understand their stiffness properties and the accuracy of predictive modeling. By simulating and examining two different sandwich structures made of Carbon fiber face sheets and Kevlar honeycomb core material represented as an equivalent solid, this study fills this gap. The Gibson and Ashby model has been adopted to find the equivalent orthotropic properties of the core because this model provides a balance between precision, computational efficiency, and suitability for honeycomb cores, guaranteeing accurate stiffness predictions and facilitating simple engineering design implementation. Experimental stiffness values of 529.74 N/mm and 479.98 N/mm for the two configurations are obtained by performing a “Three Point Bend Test” on the manufactured panels. With an accuracy deviation of about 0.84%, the numerical model predictions closely resemble the experimental findings, demonstrating the model’s dependability in representing the material’s static behavior. The sandwich structure demonstrates a stiffness of about 565 N/mm, suitable for high-load applications in aerospace and automotive sectors. Numerical modeling effectively validates the experimental results by accurately predicting the stiffness of Kevlar honeycomb core sandwich panels.</Abstract>
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			<Object Type="keyword">
			<Param Name="value">Numerical modeling</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Composite sandwich</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Kevlar® Honeycomb</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Orthotropic Properties</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Stiffness</Param>
			</Object>
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<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9796_21508b1d1867fce78a4bf07d275d34f3.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Microstructure Study and Optimization of Hardness and Tensile Strength of AW2024/B4Cp Reinforced Composites Through Linear Regression</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>83</FirstPage>
			<LastPage>96</LastPage>
			<ELocationID EIdType="pii">9667</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.36248.1781</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Bharath</FirstName>
					<LastName>Lakshminarayana</LastName>
<Affiliation>Department of Mechanical Engineering, Cambridge Institute of Technology, K R Puram, Affiliated to Visvesvaraya Technological University (V.T.U), Belagavi, Karnataka, 590 018, India</Affiliation>

</Author>
<Author>
					<FirstName>Jayappa</FirstName>
					<LastName>Kumaraswamy</LastName>
<Affiliation>Department of Electronics and Communication Engineering, R L Jalappa Institute of Technology, Affiliated to Visvesvaraya Technological University (V.T.U), Belagavi, Karnataka, 590 018, India</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>12</Month>
					<Day>14</Day>
				</PubDate>
			</History>
		<Abstract>The current research is focused on the production of AW2024/B&lt;sub&gt;4&lt;/sub&gt;C metal reinforced composite by using the liquid stir casting method. Ceramic particles armored composites are mainly used in engineering applications, which include aircraft, automotive, and marine fields. AW2024/B&lt;sub&gt;4&lt;/sub&gt;C composites are produced by changing wt.% of B&lt;sub&gt;4&lt;/sub&gt;C&lt;sub&gt;p&lt;/sub&gt; as 1.00%, 3.00% and 5.00%. The produced AW2024/B&lt;sub&gt;4&lt;/sub&gt;C composites are machined as per ASTM E8-16a, IS1500, and IS7739 standard test size and subjected to artificial ageing. The hardness and tensile strength of AW2024/B&lt;sub&gt;4&lt;/sub&gt;C composites were measured through a Brinell hardness tester and a universal testing machine, respectively. The microstructure of the prepared composite material was examined to determine the uniform distribution of reinforcement material. The highest hardness and tensile strength of AW2024/B&lt;sub&gt;4&lt;/sub&gt;C composites were measured and found to be 84.97 BHN and 273.82 N/mm&lt;sup&gt;2 &lt;/sup&gt;for AW2024/5%B&lt;sub&gt;4&lt;/sub&gt;C with 5 hrs. ageing duration. The results achieved reveal that both hardness as well as tensile strength increased by increasing the weight percentage of B&lt;sub&gt;4&lt;/sub&gt;C content. L&lt;sub&gt;9&lt;/sub&gt; standard orthogonal display was espoused to investigate the best parameter and also to authenticate the experimental test results. Further, a fracture study was done through SEM images to determine the mode of fracture.</Abstract>
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			<Param Name="value">Hardness</Param>
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<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9667_12c6a6d59730a0ae4d04c211a7893716.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Effect of Nickel Addition on the Coefficient of Thermal Expansion and Microstructural Characteristics of AA2024 and AA7175 Aluminum Alloys in As-Cast and Homogenized States</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>97</FirstPage>
			<LastPage>116</LastPage>
			<ELocationID EIdType="pii">9242</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.35302.1727</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Pagadaddinni</FirstName>
					<LastName>Rajendra</LastName>
<Affiliation>Department of Mechanical Engineering, Research Scholar, Ramaiah Institute of Technology, Bangalore, 560054, India</Affiliation>

</Author>
<Author>
					<FirstName>Sundarraju</FirstName>
					<LastName>Mohanraju Raju</LastName>
<Affiliation>Research Scholar, Department of Mechanical Engineering, Ramaiah Institute of Technology, Bangalore, 560054, India</Affiliation>

</Author>
<Author>
					<FirstName>Channegowdana Doddy Madegowda</FirstName>
					<LastName>Ramesha</LastName>
<Affiliation>Department of Mechanical Engineering, Research Scholar, Ramaiah Institute of Technology, Bangalore, 560054, India</Affiliation>
<Identifier Source="ORCID">0000-0002-5260-0513</Identifier>

</Author>
<Author>
					<FirstName>Rajarathnam</FirstName>
					<LastName>Chandrashekar</LastName>
<Affiliation>Research Consultant or Mentor, Department of Mechanical Engineering, Sambhram Institute of Technology, Bangalore, 560097, India</Affiliation>

</Author>
<Author>
					<FirstName>Nagaral</FirstName>
					<LastName>Madeva</LastName>
<Affiliation>Manager (Design) Aircraft Research and Design Centre Hindustan Aeronautics Limited, Bangalore, 560037, India</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>09</Month>
					<Day>12</Day>
				</PubDate>
			</History>
		<Abstract>Aluminum alloys are widely used in aerospace structures, necessitating continuous improvement in their mechanical properties. Micro alloying with nickel can enhance these properties and improve the coefficient of thermal expansion. This study investigates the influence of nickel on the microstructural and thermal expansion characteristics of AA2024 and AA7175 aluminum alloys, both commonly used in aerospace. AA2024 primarily contains copper, while AA7175 has zinc; both are heat-treatable and possess excellent strength. In this research, alloys were stir-cast with varying percentages of nickel and 0.2% strontium, which improves grain structure. The alloys were homogenized at 480°C for 15 hours, quenched in water, and subjected to tensile testing, EDS, XRD, and microstructural and thermal expansion analyses. Results showed that nickel addition increased strength to 215 MPa for AA2024 and 284 MPa for AA7175 with 5% nickel. XRD and EDS revealed the formation of intermetallic compounds like Al&lt;sub&gt;2&lt;/sub&gt;Ni&lt;sub&gt;3&lt;/sub&gt;, Al&lt;sub&gt;3&lt;/sub&gt;Ni, and Al&lt;sub&gt;3&lt;/sub&gt;NiCu. However, increasing nickel beyond 5% led to undesirable needle-like structures. Thermal expansion studies indicated a reduction in the coefficient of linear thermal expansion by 14.1% for AA2024 and 16.5% for AA7175 with 2% nickel, reducing thermal stress under loading up to 350°C.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Aluminium Alloys</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nickel Micro-Alloying</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Coefficient of Thermal Expansion</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Intermetallic Compounds</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Heat treatment</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Grain refinement</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9242_dadbb564426a503102ccaf9de0442626.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Large Deflection Analysis of Graphene Sheets in the Thermal Environment Using Higher-Order Nonlocal Strain Gradient Principle</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>117</FirstPage>
			<LastPage>128</LastPage>
			<ELocationID EIdType="pii">9429</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.32881.1603</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Mostafa</FirstName>
					<LastName>Sadeghian</LastName>
<Affiliation>Department of Mechanical Engineering, Faculty of Engineering, Ferdowsi University of Mashhad, Mashhad, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mahmoud</FirstName>
					<LastName>Shariati</LastName>
<Affiliation>Department of Mechanical Engineering, Faculty of Engineering, Ferdowsi University of Mashhad, Mashhad, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>01</Month>
					<Day>03</Day>
				</PubDate>
			</History>
		<Abstract>This paper investigates the large deflection of a sector nanoplate on the Winkler elastic foundation in the thermal environment based on the nonlocal strain gradient principle. By taking into account von Karman’s nonlinear strains and applying the higher-order shear deformation theory (HSDT), the governing equations of the graphene plate are derived. By presenting acceptable accuracy without the need for a shear correction coefficient, HSDT eliminates the defects of the first shear deformation theory (FSDT) and provides an appropriate distribution for shear stress along the thickness. The equations have been solved using the differential quadrature method (DQM) and the extended Kantorovich method (EKM). The results of the present study are compared with the available references, which demonstrate good agreement among them. For example, the results of the present study for the radius ratios of 0.25, 0.5, and 0.75 have 0.35%, 2.83%, and 7% differences with Ref.&lt;strong&gt; &lt;/strong&gt;[1]. In conclusion, this study examines the impact of various small-scale parameters, load, boundary conditions, geometric dimensions, and elastic foundation on the maximum nondimensional deflection in the thermal environment.</Abstract>
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			<Param Name="value">Large deflection</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Sector</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nonlocal strain gradient principle</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Thermal environment</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">HSDT</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9429_da2a932c0f4f1be0dd2ac4f49c57300d.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Statistical Analysis of Delamination Effect on Natural Frequency of Composite Laminated Plate</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>129</FirstPage>
			<LastPage>142</LastPage>
			<ELocationID EIdType="pii">9596</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.36174.1776</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Hossein</FirstName>
					<LastName>Taghavian</LastName>
<Affiliation>Department of Solid Mechanic, Faculty of Mechanical Engineering, University of Kashan, Kashan 87317-51167, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Ahmad Reza</FirstName>
					<LastName>Ghasemi</LastName>
<Affiliation>Department of Solid Mechanic, Faculty of Mechanical Engineering, University of Kashan, Kashan 87317-51167, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>12</Month>
					<Day>07</Day>
				</PubDate>
			</History>
		<Abstract>This study examines the free vibration behavior of composite laminated plates featuring various delaminated regions and stacking sequences. Utilizing the first-order shear deformation theory (FSDT) in combination with the finite element method, the natural frequencies of these plates are analyzed. Specifically, the investigation considers laminated plates with different numbers, sizes, and geometric arrangements of delaminated regions across several stacking sequences. The numerical results reveal notable trends in how natural frequencies vary and how delamination size affects them, highlighting a strong dependence on the stacking sequence of the layers. Furthermore, the findings demonstrate that the impact of multiple delaminated regions on the natural frequencies is less significant than the cumulative effect of these delaminations concentrated in a single location, with this discrepancy influenced by the frequency order and stacking configurations.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Laminated plate</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Vibration characteristics</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Delaminated regions</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">High-Risk zone ratio</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Frequency shift</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9596_30b03e9d05a4a9adab721afc7d0fa988.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Experimental Analysis of the Effect of Mechanical Topology on the Surface of Biological Microgripper Made of Ionic-Polymer Metal Composite Smart Material</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>143</FirstPage>
			<LastPage>156</LastPage>
			<ELocationID EIdType="pii">9199</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2024.33962.1670</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Hamid</FirstName>
					<LastName>Soleimanimehr</LastName>

						<AffiliationInfo>
						<Affiliation>Department of Mechanical and Aerospace Engineering, SR.C., Islamic Azad University, Tehran, Iran</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Modern Automotive Research Center, SR.C., Islamic Azad University, Tehran, Iran</Affiliation>
						</AffiliationInfo>

</Author>
<Author>
					<FirstName>Shadan</FirstName>
					<LastName>Bafandeh Haghighi</LastName>

						<AffiliationInfo>
						<Affiliation>Department of Mechanical and Aerospace Engineering, SR.C., Islamic Azad University, Tehran, Iran</Affiliation>
						</AffiliationInfo>

						<AffiliationInfo>
						<Affiliation>Modern Automotive Research Center, SR.C., Islamic Azad University, Tehran, Iran</Affiliation>
						</AffiliationInfo>

</Author>
<Author>
					<FirstName>Amin</FirstName>
					<LastName>Nasrollah</LastName>
<Affiliation>Department of Mechanical Engineering, Iran University of Science and Technology, Tehran, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>04</Month>
					<Day>29</Day>
				</PubDate>
			</History>
		<Abstract>This paper aims to discuss the electromechanical behavior of an ionic polymer metal composite (IPMC) with electrodes made of platinum and polymeric membrane made of Nafion-117 in the structure of a gripper. Two methods are used in this research; the experimental method and the finite element method. After producing an IPMC with the mentioned properties and setting the gripper structure, the generated blocking force was measured and its ability to lift and move two external specimens made of aluminum and fish egg with a radius of     m was evaluated. The Same analysis was done by the finite element method. The magnitude of the distributed load is approximately equal to . The surface area of the sample is equal to . After conducting the statistical calculations, the concentrated force on the tip of the beam is  and the results of the two methods are consistent with each other with an error of . When a concentrated force is applied to the spherical sample, both pure aluminum and fish egg materials experience an identical maximum stress of . The maximum displacement for the aluminum sample is , and for the fish egg sample, it is . It has been concluded that this gripper is able to lift and move the mentioned samples and IPMC is a biocompatible material since it is compatible with the bio-sample (fish egg) considered in this research.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Ionic polymer metal composite (IPMC)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Bio-Compatibility</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Blocking force</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">finite element method</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Experimental Method</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9199_cddc4d584be6e81ebbc2f0551f06acad.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Biodegradation, Mechanical and Physical Properties of Poly(butylene succinate) and Natural Rubber Compound Blend Filled with Activated Carbon from Coconut Fruit</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>157</FirstPage>
			<LastPage>169</LastPage>
			<ELocationID EIdType="pii">9940</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.34363.1684</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Nuan La-ong</FirstName>
					<LastName>Srakaew</LastName>
<Affiliation>Department of Materials and Medical Technology Engineering, Faculty of Engineering and Technology, Rajamangala University of Technology Isan, Nakhon Ratchasima, 30000, Thailand</Affiliation>

</Author>
<Author>
					<FirstName>Ing-orn</FirstName>
					<LastName>Sittitanadol</LastName>
<Affiliation>Department of Metallurgical Engineering, Faculty of Engineering, Rajamangala University of Technology Isan, Khon Kaen Campus, Khon Kaen, 40000, Thailand</Affiliation>

</Author>
<Author>
					<FirstName>Patcharapon</FirstName>
					<LastName>Somdee</LastName>
<Affiliation>Department of Materials and Medical Technology Engineering, Faculty of Engineering and Technology, Rajamangala University of Technology Isan, Nakhon Ratchasima, 30000, Thailand</Affiliation>

</Author>
<Author>
					<FirstName>Sombut</FirstName>
					<LastName>Noyming</LastName>
<Affiliation>Department of Materials and Medical Technology Engineering, Faculty of Engineering and Technology, Rajamangala University of Technology Isan, Nakhon Ratchasima, 30000, Thailand</Affiliation>

</Author>
<Author>
					<FirstName>Witawat</FirstName>
					<LastName>Singsang</LastName>
<Affiliation>Department of Aircraft Part Manufacturing Technology, Faculty of Industrial Technology, Rambhai Barni Rajabhat University, Chanthaburi, 22000, Thailand</Affiliation>

</Author>
<Author>
					<FirstName>Pranee</FirstName>
					<LastName>Chumsamrong</LastName>
<Affiliation>School of Polymer Engineering, Institute of Engineering, Suranaree University of Technology, Nakhon Ratchasima, 30000, Thailand</Affiliation>

</Author>
<Author>
					<FirstName>Natkrita</FirstName>
					<LastName>Prasoetsopha</LastName>
<Affiliation>Department of Materials and Medical Technology Engineering, Faculty of Engineering and Technology, Rajamangala University of Technology Isan, Nakhon Ratchasima, 30000, Thailand</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>06</Month>
					<Day>07</Day>
				</PubDate>
			</History>
		<Abstract>Activated carbon (AC) was synthesized from coconut fruit and used as a bio-filler in poly(butylene succinate) (PBS) and natural rubber compound (NRC) composites. The activation process used a potassium hydroxide (KOH) solution, followed by microwave irradiation. Two KOH concentrations (1 M and 3 M) were used, and the obtained AC was labeled AC 1 M KOH and AC 3 M KOH. The objective of this study was to examine the effects of AC type and content (0-6 phr) on the mechanical, physical, and biodegradation properties of PBS/NRC/AC composites. The results showed that AC contained 73-74 % carbon content. The AC 3 M KOH exhibited a higher surface area. The mechanical properties of PBS/NRC/AC composites, including flexural strength, impact strength, tensile strength, Young’s modulus, and elongation at fracture, tended to decrease with increasing amounts of AC. However, adding AC 3 M KOH had a more positive effect on these properties compared to AC 1 M KOH. The crystalline structure of PBS was not affected, while the melt flow index (MFI) of the composite tended to decrease with the addition of AC. The composite with 6 phr of AC 3 M KOH showed 22.4% CO₂ absorption, 35% degradation after 6 months, and 0.84% water absorption, all of which were higher than those observed for 6 phr of AC 1 M KOH. The surface morphology of PBS/NRC/AC composites had a rough appearance, with rubber particles and AC dispersed within the PBS matrix. The surface roughness intensified with increasing AC content.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Poly(butylene succinate)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Natural rubber</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Coconut</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Activated carbon</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9940_f606b6783e5451cb99b916d082f6e35c.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Influence of Process Parameters on the Mechanical Properties of Carbon Fibre Reinforced PETG</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>171</FirstPage>
			<LastPage>184</LastPage>
			<ELocationID EIdType="pii">9835</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.36494.1791</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Prabhakaran</FirstName>
					<LastName>Ramachandran</LastName>
<Affiliation>Department of Mechanical Engineering, Ramco Institute of Technology, Rajapalayam, 626 117, Tamil Nadu, India</Affiliation>

</Author>
<Author>
					<FirstName>Pitchipoo</FirstName>
					<LastName>Pandian</LastName>
<Affiliation>Department of Mechanical Engineering, P.S.R. Engineering College, Sivakasi, 626140, Tamilnadu, India</Affiliation>

</Author>
<Author>
					<FirstName>Venkatesh</FirstName>
					<LastName>Ramamoorthi</LastName>
<Affiliation>Department of Mechanical Engineering, Ramco Institute of Technology, Rajapalayam, 626 117, Tamil Nadu, India</Affiliation>

</Author>
<Author>
					<FirstName>Jerold John Britto</FirstName>
					<LastName>John</LastName>
<Affiliation>Department of Mechanical Engineering, Ramco Institute of Technology, Rajapalayam, 626 117, Tamil Nadu, India</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>01</Month>
					<Day>08</Day>
				</PubDate>
			</History>
		<Abstract>The research analyses the impact of different compositions of carbon fibre on mechanical and thermal attributes of Fused Filament Fabricated (FFF) Polyethylene Terephthalate Glycol (PETG) composites. Three different types of carbon fibre composite (10%, 20%, and 30% content) were manufactured for analysis against pure PETG material. The tests analysed the mechanical performance through compressive strength analysis, along with flexural strength measurements and measurements of hardness. The characterizing tests included Vicat Softening Temperature alongside Heat Deflection Temperature assessment. The research used ASTM standard testing methods to validate experimental measurements through finite element simulations using ANSYS Workbench ACP®. Integration of carbon fibre components improved the total mechanical behaviour of the PETG material. PETG without fibre demonstrated 53 MPa compressive strength, while 30% CF-PETG achieved 58 MPa compressive strength. The flexural strength measurements mirrored those changes, starting from 54 MPa and reaching 80 MPa across the same compositions. The Shore Hardness measurement (D) experienced an elevation as the carbon fibre concentration in materials grew from 71 to 77. Vicat Softening Temperature and Heat Deflection Temperature values improved alongside carbon fibre content increases. The experimental results matched closely with simulation outputs from the analysis, thus validating its accuracy. Research data shows that PETG materials improve their mechanical and thermal qualities when carbon fibre is incorporated, thereby creating promising prospects for specific applications needing advanced performance levels.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Carbon fibre</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Polyethylene Terephthalate Glycol (PETG)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Mechanical properties</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Thermal properties</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Fused filament fabrication (FFF)</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9835_8bb73ad27250863c02003c1ab6a23681.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Investigation of Mechanical Properties for Blend Epoxy-Polysulfide Reinforced with Woven Carbon and Glass Fiber</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>185</FirstPage>
			<LastPage>195</LastPage>
			<ELocationID EIdType="pii">9658</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.34964.1711</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Waleed Hamed</FirstName>
					<LastName>Hamza</LastName>
<Affiliation>Mechanical Engineering Department, University of Technology-Iraq, Baghdad, Iraq</Affiliation>

</Author>
<Author>
					<FirstName>Orhan Sabah</FirstName>
					<LastName>Abdullah</LastName>
<Affiliation>Mechanical Engineering Department, University of Technology-Iraq, Baghdad, Iraq</Affiliation>

</Author>
<Author>
					<FirstName>Ibtihal Abdulrazak</FirstName>
					<LastName>Mahmood</LastName>
<Affiliation>Mechanical Engineering Department, University of Technology-Iraq, Baghdad, Iraq</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>08</Month>
					<Day>06</Day>
				</PubDate>
			</History>
		<Abstract>In this work, the effect of the axial buckling load characteristics of a composite material consisting of epoxy resin (EP) and different weight percentages of polysulfide (PS) (0%, 2%, 4%, 6%, and 8%) prepared and reinforced with woven carbon and glass fibers was studied. Buckling and tensile specimens were manufactured using hand lay-up techniques according to ASTM D6641, ASTM D638, and ASTM 3039 standards. Using eight layers of fibers in three stacking sequences S1(Carbon-Carbon-Glass-Glass)x2, S2(Carbon-Glass-Carbon-Glass)x2, and S3(Carbon-Glass-Glass-Carbon)x2 and different orientation angles (0, 30, 60, and 90°), testing was performed on critical buckling load specimens by applying an axial compressive force using a testing machine. Increasing the amount of polysulfide in blends made them more flexible, but it also made the critical buckling load, tensile stress, and modulus of elasticity properties decrease compared to the pure epoxy. It was also observed that the hybrid composite material made of (EP+6% PS) reinforced with fiber improved the critical buckling load and tensile stress by (186.6%, 141%, and 219%) and (760, 698%, and 875%) when the fibers layers arranged according to (S1, S2, and S3) models, correspondingly. The experimental results obtained manifested that the best value of the critical buckling load and tensile stress at stacking sequence (CGGC)x2 was when the carbon fibers were in the direction (0–90°) and when the axial force of tension and compression was in the direction of the fibers.</Abstract>
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			<Param Name="value">Epoxy</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Polysulfide</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Carbon fiber</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Stacking sequence</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Buckling behavior</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9658_2016ee080c455bdd3fcf1c67603f77e3.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Reinforcement Surface Modification Effect on the Microstructure, Mechanical, and Tensile Fractography of Al2219 Alloy B4C Composites</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>197</FirstPage>
			<LastPage>210</LastPage>
			<ELocationID EIdType="pii">9951</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.34881.1705</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Subhashchandra</FirstName>
					<LastName>Ganiger</LastName>
<Affiliation>Department of Mechanical Engineering, B.L.D.E.A’s Dr. P. G. Halakatti College of Engineering and Technology, Vijayapur-586103, Karnataka, India</Affiliation>

</Author>
<Author>
					<FirstName>Mahadev</FirstName>
					<LastName>Sakri</LastName>
<Affiliation>Department of Mechanical Engineering, B.L.D.E.A’s Dr. P. G. Halakatti College of Engineering and Technology, Vijayapur-586103, Karnataka, India</Affiliation>

</Author>
<Author>
					<FirstName>Naveen Kumar Bannuru</FirstName>
					<LastName>Karagaiah</LastName>
<Affiliation>Department of Mechanical Engineering, M S Ramaiah Institute of Technology, Bengaluru, India</Affiliation>

</Author>
<Author>
					<FirstName>Halkur Siddagangaiah</FirstName>
					<LastName>Kumar</LastName>
<Affiliation>Department of Mechanical Engineering, Nitte (Deemed to be University), NMAM Institute of Technology, Karkala-574110, 
Karnataka, India</Affiliation>

</Author>
<Author>
					<FirstName>Manjunath Yadav</FirstName>
					<LastName>Siriyanna</LastName>
<Affiliation>Department of Mechanical Engineering, Government Engineering College, Gangavathi-583227, Karnataka, India</Affiliation>

</Author>
<Author>
					<FirstName>Vijayendra</FirstName>
					<LastName>Kukanur</LastName>
<Affiliation>Department of Mechanical Engineering, H.K.E. Society’s SiR M. Visvesvaraya College of Engineering, Raichur-584135, Karnataka, India</Affiliation>

</Author>
<Author>
					<FirstName>Madeva</FirstName>
					<LastName>Nagaral</LastName>
<Affiliation>Aircraft Research and Design Centre, Hindustan Aeronautics Limited, Bangalore-560037, Karnataka, India</Affiliation>

</Author>
<Author>
					<FirstName>Fazil</FirstName>
					<LastName>Nalband</LastName>
<Affiliation>Department of Mechanical Engineering, Ballari Institute of Technology and Management, Ballari, Karnataka, India</Affiliation>

</Author>
<Author>
					<FirstName>Virupaxi</FirstName>
					<LastName>Auradi</LastName>
<Affiliation>Department of Mechanical Engineering, Siddaganga Institute of Technology, Tumakuru-572103, Karnataka, India</Affiliation>

</Author>
<Author>
					<FirstName>Nagaraj</FirstName>
					<LastName>Namdev</LastName>
<Affiliation>Department of Mechanical Engineering, APS Polytechnic, Bangalore-560082, Karnataka, India</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>07</Month>
					<Day>28</Day>
				</PubDate>
			</History>
		<Abstract>Al2219 alloy composites were produced through the stir cast process, with varying amounts of copper-coated B&lt;sub&gt;4&lt;/sub&gt;C particles (2%, 4%, 6%, 8%, and 10%) incorporated. The mechanical performance of surface-modified B&lt;sub&gt;4&lt;/sub&gt;C additions to Al2219 alloy was examined by conducting tensile tests on the prepared composites. The synthesized composites&#039; microstructural, mechanical, and tensile fractured surfaces were evaluated. Characterization of the samples&#039; microstructure using SEM microscopy and EDS patterns. B&lt;sub&gt;4&lt;/sub&gt;C particle existence was verified by the EDS findings. The inclusion of Cu-coated B&lt;sub&gt;4&lt;/sub&gt;C reinforcement enhanced the hardness, tensile, and bending strength of the metal composite in contrast to the uncoated B&lt;sub&gt;4&lt;/sub&gt;C particles. Hardness of Al2219 alloy was improved by 92.4% with the 10 wt.% of Cu coated B&lt;sub&gt;4&lt;/sub&gt;C in the Al matrix. Further, there was a 73.5 % improvement in the ultimate strength. The Al2219 alloy composite&#039;s ductility decreased with the reinforcement&#039;s incorporation. Tensile fractured surfaces SEM micrographs show strong bonding between the matrix and boron carbide particles. The particle shear was observed in the case of copper-coated B&lt;sub&gt;4&lt;/sub&gt;C reinforced composites due to increased wettability. Various fractured surfaces were studied using SEM micrographs to determine fracture mechanisms in composites.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Al alloy</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Boron Carbide</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Stir Casting</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Electroless Coating</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">tensile strength</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9951_0779b1428243e4e11ab7f77d8b9a34fb.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Enhancing Mechanical Properties of Polypropylene Composites Reinforced with Date Palm Fiber Using Maleic Anhydride Grafted Polypropylene as a Compatibilizer</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>211</FirstPage>
			<LastPage>226</LastPage>
			<ELocationID EIdType="pii">9665</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.35464.1736</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Saeed</FirstName>
					<LastName>Ghorbani</LastName>
<Affiliation>Faculty of Mechanical Engineering, Semnan University, Semnan, 35131-19111, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mohammad</FirstName>
					<LastName>Nouri Damghani</LastName>
<Affiliation>Faculty of Mechanical Engineering, Semnan University, Semnan, 35131-19111, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Hossein</FirstName>
					<LastName>Taghipoor</LastName>
<Affiliation>Faculty of Mechanical Engineering, Velayat University, Iranshahr, 99111-31311, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>09</Month>
					<Day>29</Day>
				</PubDate>
			</History>
		<Abstract>This study investigates the effects of incorporating date palm fiber (DPF), polypropylene grafted maleic anhydride (PP-g-MA), and impact-modifying masterbatch on the tensile properties of polypropylene (PP) composites. Using a design of experiments (DOE) approach and analysis of variance (ANOVA), the interactions between these components were analyzed. The tensile strength of the composites increased by up to 21.08% compared to pure PP, reaching 19.6 MPa, while the elastic modulus improved by 54.78%, reaching 2.43 GPa, at 20 wt.% DPF and 5 wt.% PP-g-MA. Although the masterbatch enhanced impact resistance, its higher concentrations reduced tensile strength by up to 31.97% compared to formulations with minimal masterbatch content. The optimal composition—20 wt.% DPF, 5 wt.% PP-g-MA, and 1 wt.% masterbatch—exhibited the best overall mechanical performance, balancing tensile strength, elastic modulus, and impact resistance. This study highlights the synergistic effects of natural fibers and polymer compatibilizers, providing a pathway for the development of sustainable, high-performance bio-composites.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Date Palm Fiber</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Composite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">compatibilizer</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Bio-composite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">mechanical property</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9665_0af3047bfab199ed6fcf61662cb1edee.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>A Finite Element Formulation for Analyzing the Nonlinear Static Response of Bi-functionally Graded Microbeam Resting on Elastic Foundation Under Various Loads</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>227</FirstPage>
			<LastPage>243</LastPage>
			<ELocationID EIdType="pii">9838</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.37288.1828</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Van-Chinh</FirstName>
					<LastName>Nguyen</LastName>
<Affiliation>Faculty of Mechanical Engineering, Le Quy Don Technical University, Hanoi, Vietnam,</Affiliation>

</Author>
<Author>
					<FirstName>Trung Thanh</FirstName>
					<LastName>Tran</LastName>
<Affiliation>Faculty of Mechanical Engineering, Le Quy Don Technical University, Hanoi, Vietnam,</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>04</Month>
					<Day>02</Day>
				</PubDate>
			</History>
		<Abstract>The main goal of this paper is to introduce a finite element formulation to investigate the nonlinear static response of the 2DFG-McrB resting on EF under four different loads. The governing equations are established using the principle of minimum potential energy, incorporating the RBT and geometric nonlinearity based on the von Kármán assumptions. A weak-form finite element method is developed and solved iteratively through the Newton-Raphson method. The proposed formulation is validated against benchmark results from the literature, demonstrating its accuracy and computational efficiency. Furthermore, a comprehensive parametric study is conducted to evaluate the effects of geometrical dimensions, material properties, foundation stiffness, length-scale parameters, and BCs on the nonlinear response of 2DFG-McrBs. The findings provide valuable insights for the design and analysis of McrBs in engineering applications and serve as a basis for future studies on advanced microstructures.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Microbeam</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">2D-FGM</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Elastic foundation</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">nonlinear bending</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9838_2d5b22e575c6a28b0023514dd22f486d.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>13</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2026</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Applying an Artificial Neural Network to Predict the Mechanical Properties of Epoxy Resin with Graphite Additive After Water Absorption</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>245</FirstPage>
			<LastPage>257</LastPage>
			<ELocationID EIdType="pii">9839</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2025.37083.1814</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Mohammad Amin</FirstName>
					<LastName>Torabizadeh</LastName>
<Affiliation>Department of Industrial, University of Applied Science and Technology, Tehran, 91379-33435, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Abdolhosein</FirstName>
					<LastName>Fereidoon</LastName>
<Affiliation>Faculty of Mechanical Engineering, Semnan University, Semnan, 35131-19111, Iran</Affiliation>
<Identifier Source="ORCID">0000-0002-3791-6528</Identifier>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>04</Month>
					<Day>03</Day>
				</PubDate>
			</History>
		<Abstract>The present study utilized an artificial neural network (ANN) model to anticipate Barcol hardness, impact strength, and heat deflection temperature data for epoxy resin specimens with varying weight percentages of graphite additive exposed in different types of water. A feedforward backpropagation algorithm was used for predictive modeling with two input parameters: the weight percentage of the graphite additive (0, 5, 10, 15, and 25 wt.%) and the type of water used (dry specimen, potable water, distilled water, alkaline solution, and acidic solution). Experimental test data for mechanical properties were used to train the ANN model. The network was validated by comparing the predicted outputs with experimental data and by evaluating performance metrics. The results conclude that the ANN model is a practical and accurate approach for rapidly predicting mechanical performance and can be considered a substitute for traditional procedures used to characterize composite materials through experimental methods. Among the two input parameters, the weight percentage of the graphite additive was the most essential input parameter used to predict the mechanical properties of composites. Besides, the key findings of this work can also be a reference for the engineering practice of composite materials under mechanical and moisture environments.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Artificial Neural Network</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Graphite additive</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Polymer composites</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Water absorption</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Mechanical properties</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_9839_0fefef0f7605e843234a47f89867fec0.pdf</ArchiveCopySource>
</Article>
</ArticleSet>
