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<ArticleSet>
<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Experimental investigation of the strength of glass fiber-reinforced concrete exposed to high temperature</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>103</FirstPage>
			<LastPage>113</LastPage>
			<ELocationID EIdType="pii">3282</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.1264.1056</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Amir Hamzeh</FirstName>
					<LastName>Keykha</LastName>
<Affiliation>Department of Civil Engineering, Faculty of Engineering, Zahedan Branch, Islamic Azad University, Zahedan, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2017</Year>
					<Month>03</Month>
					<Day>13</Day>
				</PubDate>
			</History>
		<Abstract>This study investigated the effects of high temperature exposure on the compressive, tensile, and flexural strengths of concrete containing glass fiber. A total of 108 cubic specimens (150 mm × 150 mm × 150 mm), cylindrical specimens (300 mm × 150 mm), and prismatic specimens (500 mm × 150 mm × 150 mm) were prepared for compressive, tensile, and flexural strength testing, respectively. The specimens were incorporated with 1%, 2%, and 3% glass fiber and cured for 28 days to derive the desired strengths. The specimens were then annealed and subjected to experiments in which they were exposed to high temperature (600°C) for 30 minutes, one hour, and two hours. The specimens were cooled via slow cooling (exposure to air) and fast cooling (water spraying immediately after exposure to heat). Results showed that the presence of glass fiber exerted different effects on specimen strength and that heat caused the formation of numerous cracks in the specimens.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">High temperature</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Glass fiber</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Concrete</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Experimental investigation</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3282_6b3ccbfc4abf1c2c0d15ec32749d073b.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Optimization of infinite composite plates with quasi-triangular holes under in-plane loading</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>115</FirstPage>
			<LastPage>130</LastPage>
			<ELocationID EIdType="pii">3283</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.1749.1088</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Seyed Ahmad</FirstName>
					<LastName>Mahmodzade Hoseyni</LastName>
<Affiliation>Shahrood university of technology</Affiliation>

</Author>
<Author>
					<FirstName>Mohammad</FirstName>
					<LastName>Jafari</LastName>
<Affiliation>Department of Mechanical Engineering, University of shahrood</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2016</Year>
					<Month>11</Month>
					<Day>20</Day>
				</PubDate>
			</History>
		<Abstract>This study used particle swarm optimization (PSO) to determine the optimal values of effective design variables acting on the stress distribution around a quasi-triangular hole in an infinite orthotropic plate. These parameters were load angle, hole orientation, bluntness, fiber angle, and material properties, which were ascertained on the basis of an analytical method used by Lekhnitskii [3]. The cost function was regarded as the maximum stress created around the hole and was calculated using the aforementioned analytical approach. The finite element method was then employed to verify the results of the analytical calculation. The overlap in the analytical and FEM calculations confirmed the validity of the solution proposed in this research. The findings further indicated that the design variables significantly affect the stress distribution around quasi-triangular holes and structural load-bearing capacity. The performance of the PSO algorithm was also investigated.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Infinite orthotropic plate</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Quasi-triangular hole</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Particle swarm optimization</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Analytical Solution</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Complex variable method</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3283_cdbb99113dda990fa7f50b13633a876c.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Effects of reinforcement distribution on the mechanical properties of Al–Fe3O4 nanocomposites fabricated via accumulative roll bonding</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>131</FirstPage>
			<LastPage>139</LastPage>
			<ELocationID EIdType="pii">3284</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.12290.1121</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Behrooz</FirstName>
					<LastName>Pirouzi</LastName>
<Affiliation>Dep. of Nanotechnology, Nano materials group, Semnan university</Affiliation>

</Author>
<Author>
					<FirstName>Ehsan</FirstName>
					<LastName>Borhani</LastName>
<Affiliation>Semnan University</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2017</Year>
					<Month>08</Month>
					<Day>21</Day>
				</PubDate>
			</History>
		<Abstract>This research developed new nanostructured Al–Fe&lt;sub&gt;3&lt;/sub&gt;O&lt;sub&gt;4&lt;/sub&gt; composites via accumulative roll bonding (ARB). X-ray diffraction (XRD) analysis and field emission scanning electron microscopy were conducted to examine microstructural characteristics and particle distribution in the nanocomposites. Hardness and tensile strength tests were employed to examine their mechanical properties. After eight cycles of XRD analysis, the size of the Al crystals in the nanocomposites reached 198 nm. After eight cycles of tests on mechanical properties, the Al crystals exhibited a tensile strength and a hardness of 204 MPa and 63 HV, respectively. These values are higher than those achieved by pure Al. The depth of nanocomposite rupture observed in fractographic analysis revealed that a ductile fracture occurred in the materials because of the formation and growth of cavities.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Metal matrix composite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Fe3O4</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Accumulative roll bonding</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Microstructure</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Mechanical properties</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Fractography</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3284_c1bc54a32ae0c481e1a63c6a065ee102.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Creep Strain and Stress Analysis in Laminated Composite Pres-sure Vessels</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>141</FirstPage>
			<LastPage>147</LastPage>
			<ELocationID EIdType="pii">3286</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.12562.1125</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Ahmad Reza</FirstName>
					<LastName>Ghasemi</LastName>
<Affiliation>Faculty of Mechanical Engineering, University of Kashan, Kashan</Affiliation>

</Author>
<Author>
					<FirstName>Komeil</FirstName>
					<LastName>Hosseinpour</LastName>
<Affiliation>Faculty of Mechanical Engineering, University of Kashan, Kashan</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2017</Year>
					<Month>09</Month>
					<Day>21</Day>
				</PubDate>
			</History>
		<Abstract>This study investigates the time-dependent long-term creep strain in a composite cylinder made of glass/vinylester with a unidirectional ply. The cylinder is subjected to an internal pressure and the boundary condition is free–free and acts as thermal insulation. The classical lamination theory (CLT) is used to derive the governing equations as a second-order equation to determine the radial, circum-ferential, axial, and effective stresses in the cylinder wall. The distribution of the radial and circumferential creep strains is based on the Schapery’s single integral model for nonlinear viscoelastic materials. This study focuses on the effect of the orientation of the fibers on the creep strain distribution in the wall of a cylinder. The results show that the creep strain is lower when  than at . As the angle of the fibers increases, the distribution of the creep strain becomes more uniform.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Long-term creep strain</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Schapery single integral</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nonlinear viscoelastic</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Polymer matrix composites</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3286_ad1f89ee5cc286e9f6617b8fdc236a94.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Flexural Behavior of Fiber–Metal Laminates Reinforced with Surface-Functionalized Nanoclay</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>149</FirstPage>
			<LastPage>156</LastPage>
			<ELocationID EIdType="pii">3287</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.13315.1130</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Sh.</FirstName>
					<LastName>Vahedi</LastName>
<Affiliation>Materials Science and Engineering Faculty, K.N. Toosi University of Technology, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>S.M.H.</FirstName>
					<LastName>Siadati</LastName>
<Affiliation>Materials Science and Engineering Faculty, K.N. Toosi University of Technology, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>H.</FirstName>
					<LastName>Khosravi</LastName>
<Affiliation>Department of Materials Engineering, Faculty of Engineering, University of Sistan and Baluchestan, Zahedan, Iran</Affiliation>

</Author>
<Author>
					<FirstName>A.</FirstName>
					<LastName>Shahrabi</LastName>
<Affiliation>Materials Science and Engineering Faculty, K.N. Toosi University of Technology, Tehran, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2017</Year>
					<Month>12</Month>
					<Day>07</Day>
				</PubDate>
			</History>
		<Abstract>The effects of surface-functionalized Na&lt;sup&gt;+&lt;/sup&gt;-montmorillonite nanoclay particles on the flexural behavior of E-glass fiber-reinforced aluminum (GLARE) laminates were investigated. The nanoclay particles were subjected to surface functionalization using 3-(trimethoxysilyl)propylamine to increase their compatibility with the epoxy matrix and improve their dispersion within the matrix. Experimental results indicated that the GLARE laminates achieved the highest flexural strength (61%) and energy absorption (51%) at an addition of 3 wt% functionalized nanoclay. The highest flexural modulus (67% increase) was observed at an addition of 5 wt% functionalized nanoclay. The flexural properties of the functionalized nanoclay-filled GLARE laminates were significantly better than those of untreated nanoclay-filled GLARE laminates. Microscopic observations suggested that the introduction of functionalized nanoclay particles markedly enhanced the interfacial adhesion between the matrix and the E-glass fibers.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Fiber-metal laminates</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nanoclay</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Surface functionalization</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Three-point bending test</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Fracture surface</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3287_df2567a1cf2cae87d5211c4c055343d5.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Improving the Performance of Porous Concrete Composites Using Zeolite as a Coarse Grain</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>157</FirstPage>
			<LastPage>163</LastPage>
			<ELocationID EIdType="pii">3288</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.13363.1131</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Mahsa</FirstName>
					<LastName>Doostmohamadi</LastName>
<Affiliation>Graduated MSc. Student, Faculty of Civil Engineering, Semnan University, Semnan, Iran.</Affiliation>

</Author>
<Author>
					<FirstName>Hojat</FirstName>
					<LastName>Karami</LastName>
<Affiliation>Assistant Professor, Faculty of Civil Engineering, Semnan University, Semnan, Iran.</Affiliation>

</Author>
<Author>
					<FirstName>Saeed</FirstName>
					<LastName>Farzin</LastName>
<Affiliation>Assistant Professor, Faculty of Civil Engineering, Semnan University, Semnan, Iran.</Affiliation>

</Author>
<Author>
					<FirstName>Sayed-Farhad</FirstName>
					<LastName>Mousavi</LastName>
<Affiliation>Professor, Faculty of Civil Engineering, Semnan University, Semnan, Iran.</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2017</Year>
					<Month>12</Month>
					<Day>11</Day>
				</PubDate>
			</History>
		<Abstract>Porous concrete is a mixture of cement and water that may contain fine grains, which play a role in water transfer and permeability. Porous concrete can act as a drain to pass rainwater and recharge groundwater. In this study, 25%, 50%, 75%, and 100% zeolite were used to replace the coarse aggregates in porous concrete. The effects of the zeolite on the compressive strength, permeability coefficient, porosity, and density of the concrete were investigated. The results showed that the zeolite reduced the compressive strength of the concrete samples because of its porous nature. The permeability coefficient and porosity increased with the addition of zeolite. The highest (10.29 MPa) and lowest compressive strength (6.79 MPa) were observed in the 25% and 100% zeolite samples, respectively. The highest porosity (30.97%) and permeability coefficient (1.76 mm/s) were measured in the 100% zeolite sample. For the 25%, 50%, 75%, and 100% zeolite samples, the permeability coefficient increased by 6.99%, 17.39%, 21.3%, and 24.4%, respectively; the density decreased by 7.77%, 10, 15%, and 19.44%, respectively, with respect to the control sample.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Porous concrete</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Additive</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Zeolite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Physical properties</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Groundwater recharge</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3288_c78e8224a1fbc8ad836bf19207daa88e.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Investigation of Capsulated Epoxy and DCPD in Epoxy Based Self-healing Composites - DFT Calculation and Experimental Analysis</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>165</FirstPage>
			<LastPage>171</LastPage>
			<ELocationID EIdType="pii">3291</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.15389.1152</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Sepide</FirstName>
					<LastName>Khostavan</LastName>
<Affiliation>Department of chemistry, Faculty of sience, University of Semnan , Semnan,  Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mostafa</FirstName>
					<LastName>Fazli</LastName>
<Affiliation>Department of chemistry, Faculty of sience, University of Semnan , Semnan, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Abdollah</FirstName>
					<LastName>Omrani</LastName>
<Affiliation>Department of Physical Chemistry , Faculty of Chemistry, University of Mazandaran, Babolsar, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Morteza</FirstName>
					<LastName>Ghorbanzadeh Ahangari</LastName>
<Affiliation>University of Mazandaran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2018</Year>
					<Month>07</Month>
					<Day>13</Day>
				</PubDate>
			</History>
		<Abstract>Epoxy and dicyclopentadien (DCPD) are two common healing agents, which are introduced into epoxy matrix through encapsulation in order to prepare self-healing composites. In a comparative study, the compatibility of healing agents and epoxy matrix is investigated through experimental tests and DFT calculations. The interaction energy is considered to be the determinative parameter in DFT calculation. The values of total interaction energy are -0.14eV for DCPD and +0.169eV for epoxy absorbing on epoxy matrix. According to the obtained results from DFT, an attraction between DCPD and epoxy matrix is observed. DOS and charge analysis of these systems are fulfilled and demonstrated the charge transfer of 0.07 e from epoxy to DCPD. The obtained data reveal the most charge transfer is occurred in DCPD-epoxy, which affects the mechanical properties of healed composites. To examine the mechanical properties, tensile strength parameters are measured experimentally and demonstrated the improved ultimate strength of 783.49 MPa in DCPD/epoxy system rather than the ultimate strength of 571.87 MPa in epoxy/epoxy system. Also elongation at break in DCPD-epoxy system is improved to 3.44% compared to 1.84% in epoxy/ epoxy blend. These findings highlight the role of interaction energy in mechanical properties of polymeric interface, and prompt further experiments and simulations to confirm this effect.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Epoxy</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">DCPD</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">DFT</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">interaction energy</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">tensile strength</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3291_674d0a1ecb40dc8e45fe43f0d752eec6.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>An Analytical Approach to Thermoelastic Bending of Simply Supported Advanced Ribbed Composite Plates</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>173</FirstPage>
			<LastPage>185</LastPage>
			<ELocationID EIdType="pii">3285</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.12357.1124</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Morteza</FirstName>
					<LastName>Shahravi</LastName>
<Affiliation>Department of Aerospace Eng.</Affiliation>

</Author>
<Author>
					<FirstName>Sina</FirstName>
					<LastName>Falahzade</LastName>
<Affiliation>department of SGC</Affiliation>

</Author>
<Author>
					<FirstName>Madhid</FirstName>
					<LastName>Mokhtari</LastName>
<Affiliation>S.G. center of research</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2017</Year>
					<Month>08</Month>
					<Day>30</Day>
				</PubDate>
			</History>
		<Abstract>In the present paper, an analytical approach is used to study the thermal deflections of a simply supported composite plate with a beam-like stiffener. The results for a plate–beam system exposed to a sinusoidal thermal load is used to study the effects of the low Earth orbit (LEO) thermal conditions on the composite plates, which have been used in the structure of satellites and spacecraft. To solve the governing equations of the system, the Laplace transform method for the time domain is used with the Navier series expansions. As the employed method is completely analytical, the results are exact.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Ribbed composite plate</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Thermoelastic Bending</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Laplace transform</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Advanced composite</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3285_21c0427816f32ae920e9c4fd078c9f24.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Semnan University Press</PublisherName>
				<JournalTitle>Mechanics of Advanced Composite Structures</JournalTitle>
				<Issn>2423-4826</Issn>
				<Volume>5</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>11</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Thermoelastic Interaction in a Three-Dimensional Layered Sandwich Structure</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>187</FirstPage>
			<LastPage>198</LastPage>
			<ELocationID EIdType="pii">3290</ELocationID>
			
<ELocationID EIdType="doi">10.22075/macs.2018.14201.1141</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Abhik</FirstName>
					<LastName>Sur</LastName>
<Affiliation>Department of Applied Mathematics, University of Calcutta, India</Affiliation>

</Author>
<Author>
					<FirstName>M.</FirstName>
					<LastName>Kanoria</LastName>
<Affiliation>Department of Applied Mathematics, University of Calcutta, India</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2018</Year>
					<Month>03</Month>
					<Day>05</Day>
				</PubDate>
			</History>
		<Abstract>The present article investigates the thermoelastic interaction in a three-dimensional homogeneous and isotropic sandwich structure using the dual-phase-lag (DPL) model of generalized thermoelasticity. The incorporated resulting non-dimensional coupled equations are applied to a specific problem in which a sandwich layer of unidentical homogeneous and isotropic substances is subjected to time-dependent thermal loadings; the two outer sides are traction-free. The analytical expressions for the displacement components, stress, temperature, and strain are obtained in the physical domain using the normal mode analysis. The mathematical difficulties in dealing with the hyperbolic heat conduction equation are overcome and the thermophysical quantities of the sandwich structure are depicted graphically. The effect that the two phase lags have on the studied field are highlighted. The results demonstrate the phenomenon of a finite speed of wave propagation in a sandwich structure for each field.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Generalized thermoelasticity</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Dual-phase-lag thermoelastic model</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Hyperbolic heat conduction</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Finite wave speed</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Normal mode analysis</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://macs.semnan.ac.ir/article_3290_c3a227cc8e384519454159e98561e0b3.pdf</ArchiveCopySource>
</Article>
</ArticleSet>
