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<ArticleSet>
<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>56</Volume>
				<Issue>5</Issue>
				<PubDate PubStatus="epublish">
					<Year>2024</Year>
					<Month>07</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Free Vibration analysis of a rotating cylindrical shell made of FG-GPLR porous core and MEE face  with uncertain parameters in thermal environment</ArticleTitle>
<VernacularTitle>Free Vibration analysis of a rotating cylindrical shell made of FG-GPLR porous core and MEE face  with uncertain parameters in thermal environment</VernacularTitle>
			<FirstPage>623</FirstPage>
			<LastPage>650</LastPage>
			<ELocationID EIdType="pii">5533</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2024.22228.7586</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Mohsen</FirstName>
					<LastName>Khanahmadi</LastName>
<Affiliation>Department of Mechanic, central Tehran Branch, Islamic Azad University, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Armen</FirstName>
					<LastName>Adamian</LastName>
<Affiliation>Islamic Azad University Tehran Central Branch</Affiliation>

</Author>
<Author>
					<FirstName>Ahmad</FirstName>
					<LastName>Hosseini-Sianaki</LastName>
<Affiliation>Mechanical Engineering, Islamic Azad University, Central Tehran Branch</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2023</Year>
					<Month>03</Month>
					<Day>02</Day>
				</PubDate>
			</History>
		<Abstract>In this study, free vibration analysis of a rotating composite double-layer cylindrical shell has been carried out using first-order shear deformation theory. The shell is made of a thin magneto-electroelastic (MEE) top layer bonded to the functionally graded graphene platelet reinforced (FG-GPLR) porous layer and is subjected to the thermal environment. The two ends of the shell can be considered as pinned boundary conditions due to the presence of bearings that prevent transverse movement. At first, natural frequencies of the forward and backward modes for the rotating composite shell were obtained and verified by the literature results. Then the effect of rotational speed, mode numbers, temperature change, porosity and GPLs mass fraction on the frequencies were investigated. This study then seeks to investigate the effect of uncertainties in the MEE layer properties on the free vibration of a rotating composite shell exposed to electric and magnetic potentials. In this case, the uncertainties in the elastic modulus, piezoelectric and piezomagnetic coefficient of the smart layer, are introduced using a symmetric Gaussian fuzzy number. The governing equations for the uncertain system are obtained by combining Hamilton&#039;s principle and the dual parametric form of fuzzy numbers; Then the natural frequencies of the uncertain model are calculated using Navier&#039;s approach. Free vibration is also investigated by obtaining the natural frequency borders with respect to the various uncertain parameters. The results have shown that the porosity increased the frequencies. In the case of uncertain properties, with increasing of the electric potential, the frequency bounds decreased slightly, but they increased intensely with increasing of the magnetic potential.</Abstract>
			<OtherAbstract Language="FA">In this study, free vibration analysis of a rotating composite double-layer cylindrical shell has been carried out using first-order shear deformation theory. The shell is made of a thin magneto-electroelastic (MEE) top layer bonded to the functionally graded graphene platelet reinforced (FG-GPLR) porous layer and is subjected to the thermal environment. The two ends of the shell can be considered as pinned boundary conditions due to the presence of bearings that prevent transverse movement. At first, natural frequencies of the forward and backward modes for the rotating composite shell were obtained and verified by the literature results. Then the effect of rotational speed, mode numbers, temperature change, porosity and GPLs mass fraction on the frequencies were investigated. This study then seeks to investigate the effect of uncertainties in the MEE layer properties on the free vibration of a rotating composite shell exposed to electric and magnetic potentials. In this case, the uncertainties in the elastic modulus, piezoelectric and piezomagnetic coefficient of the smart layer, are introduced using a symmetric Gaussian fuzzy number. The governing equations for the uncertain system are obtained by combining Hamilton&#039;s principle and the dual parametric form of fuzzy numbers; Then the natural frequencies of the uncertain model are calculated using Navier&#039;s approach. Free vibration is also investigated by obtaining the natural frequency borders with respect to the various uncertain parameters. The results have shown that the porosity increased the frequencies. In the case of uncertain properties, with increasing of the electric potential, the frequency bounds decreased slightly, but they increased intensely with increasing of the magnetic potential.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Rotating composite cylindrical shell</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Magneto-Electro-Elastic layer</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">FG-GPLR porous material</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Natural frequency</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Uncertain parameters</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_5533_8965f76632d7672e7d3cf29c87ecaa0c.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>56</Volume>
				<Issue>5</Issue>
				<PubDate PubStatus="epublish">
					<Year>2024</Year>
					<Month>07</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Redesign of energy recovery device to keep the production recovery constant</ArticleTitle>
<VernacularTitle>Redesign of energy recovery device to keep the production recovery constant</VernacularTitle>
			<FirstPage>651</FirstPage>
			<LastPage>678</LastPage>
			<ELocationID EIdType="pii">5534</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2024.22968.7705</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Abdollah</FirstName>
					<LastName>Eskandari</LastName>
<Affiliation>Payame Noor University - Faculty of Engineering</Affiliation>
<Identifier Source="ORCID">0000-0003-4441-6473</Identifier>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>02</Month>
					<Day>09</Day>
				</PubDate>
			</History>
		<Abstract>&lt;span style=&quot;letter-spacing: .05pt;&quot;&gt;One of the problems of producing fresh water by reverse osmosis is its sensitivity to process conditions. In this article, a method for redesigning the hydraulic turbocharger rotor as an energy Recovery device in desalination units has been discussed. For this purpose, firstly, the performance of a desalination unit in operation is investigated. Then, using turbomachinery similarity relations and CFD, two new rotors have been designed for two high- and low-pressure modes and replaced with the primary rotor. The validated results with the test show that despite changing membrane inlet pressure, the amount of produced water was not changed, the total efficiency has increased by more than 4% and the energy recovery has increased by about 2% in the high-pressure mode, which shows that this method can be used in situations where the pressure change of the membranes is noticeably higher or lower than the initial design pressure.&lt;/span&gt;</Abstract>
			<OtherAbstract Language="FA">&lt;span style=&quot;letter-spacing: .05pt;&quot;&gt;One of the problems of producing fresh water by reverse osmosis is its sensitivity to process conditions. In this article, a method for redesigning the hydraulic turbocharger rotor as an energy Recovery device in desalination units has been discussed. For this purpose, firstly, the performance of a desalination unit in operation is investigated. Then, using turbomachinery similarity relations and CFD, two new rotors have been designed for two high- and low-pressure modes and replaced with the primary rotor. The validated results with the test show that despite changing membrane inlet pressure, the amount of produced water was not changed, the total efficiency has increased by more than 4% and the energy recovery has increased by about 2% in the high-pressure mode, which shows that this method can be used in situations where the pressure change of the membranes is noticeably higher or lower than the initial design pressure.&lt;/span&gt;</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Reverse osmosis</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">permeate water</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Energy Recovery</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">hydraulic turbocharger</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">CFD</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_5534_de6b1cf3fb0a3aa1244d30f7b8c29c41.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>56</Volume>
				<Issue>5</Issue>
				<PubDate PubStatus="epublish">
					<Year>2024</Year>
					<Month>07</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Experimental Investigation of the Frequency Spectra of Vortex Shedding from a Triangular Bluff Body at Different Flow Angles</ArticleTitle>
<VernacularTitle>Experimental Investigation of the Frequency Spectra of Vortex Shedding from a Triangular Bluff Body at Different Flow Angles</VernacularTitle>
			<FirstPage>679</FirstPage>
			<LastPage>698</LastPage>
			<ELocationID EIdType="pii">5544</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2024.23245.7733</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Ehsan</FirstName>
					<LastName>Ardekani</LastName>
<Affiliation>Department of Mechanical Engineering, Iranian Research Organization for Science and Technology (IROST), Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Foad</FirstName>
					<LastName>Farhani</LastName>
<Affiliation>Department of Mechanical Engineering, Iranian Research Organization for Science and Technology (IROST), Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mohammad Ali</FirstName>
					<LastName>Ardakani</LastName>
<Affiliation>Department of Mechanical Engineering, Iranian Research Organization for Science and Technology (IROST), Tehran, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>06</Month>
					<Day>03</Day>
				</PubDate>
			</History>
		<Abstract>The base of the vortex flowmeter is the linear relationship  ( is a constant and  is vortex shedding frequency). Therefore, the accuracy of the flow meter is only a function of the vortex shedding frequency measurement accuracy. To determine the frequency measurement accuracy, it is necessary to investigate its frequency spectrum. In this research, vortex shedding and its frequency spectrum downstream of an equilateral triangular model of 10 mm side have been investigated experimentally in a closed-type wind tunnel using a hot-wire anemometer. The vortex shedding frequency spectra were fitted using the normal Gauss distribution, and based on the expected confidence level, the accuracy of the frequency measurement was evaluated and its changes were quantified using the standard deviation of the normal distribution. Results show for Re &gt;1200, the Strouhal number variation is independent of the Re number, and it is only a function of the flow angle. Also, for a 95% confidence level, the maximum frequency measurement error for the triangular model is 1.53% for and 2.46% for . The standard deviation of the frequency spectra has an increasing trend streamwise, however, it is constant spanwise outside the wake region. When the flow angle is in the range of , the measurement error increases to about 9%.</Abstract>
			<OtherAbstract Language="FA">The base of the vortex flowmeter is the linear relationship  ( is a constant and  is vortex shedding frequency). Therefore, the accuracy of the flow meter is only a function of the vortex shedding frequency measurement accuracy. To determine the frequency measurement accuracy, it is necessary to investigate its frequency spectrum. In this research, vortex shedding and its frequency spectrum downstream of an equilateral triangular model of 10 mm side have been investigated experimentally in a closed-type wind tunnel using a hot-wire anemometer. The vortex shedding frequency spectra were fitted using the normal Gauss distribution, and based on the expected confidence level, the accuracy of the frequency measurement was evaluated and its changes were quantified using the standard deviation of the normal distribution. Results show for Re &gt;1200, the Strouhal number variation is independent of the Re number, and it is only a function of the flow angle. Also, for a 95% confidence level, the maximum frequency measurement error for the triangular model is 1.53% for and 2.46% for . The standard deviation of the frequency spectra has an increasing trend streamwise, however, it is constant spanwise outside the wake region. When the flow angle is in the range of , the measurement error increases to about 9%.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Hot-wire anemometer</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Strouhal Number</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Triangular model</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Vortex flowmeter</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Vortex shedding frequency spectrum</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_5544_97785e0500ad16c18574c64189ccf4b4.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>56</Volume>
				<Issue>5</Issue>
				<PubDate PubStatus="epublish">
					<Year>2024</Year>
					<Month>07</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Comparison of Perceptron and Radial Basis Function Neural Networks in Modeling Heat Exchangers with Rectangular Helical Channels</ArticleTitle>
<VernacularTitle>Comparison of Perceptron and Radial Basis Function Neural Networks in Modeling Heat Exchangers with Rectangular Helical Channels</VernacularTitle>
			<FirstPage>699</FirstPage>
			<LastPage>716</LastPage>
			<ELocationID EIdType="pii">5561</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2024.22833.7684</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Reza</FirstName>
					<LastName>Beigzadeh</LastName>
<Affiliation>Department of Chemical Engineering, Faculty of Engineering, University of Kurdistan, Sanandaj, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2023</Year>
					<Month>12</Month>
					<Day>02</Day>
				</PubDate>
			</History>
		<Abstract>&lt;span style=&quot;letter-spacing: .05pt;&quot;&gt;In this research, computational fluid dynamics method was used to investigate the effect of geometrical parameters of rectangular spiral channels on heat transfer coefficient. Two artificial neural networks including perceptron (MLP) and radial basis function (RBF) models were used to model the heat transfer in helical channels. The model inputs included the Reynolds number and geometric parameters of the channels, and output was the Nusselt number. 135 data were generated by Computational Fluid Dynamics (CFD) simulation and after validation were used for training and evaluation of neural network models. The results of the research showed that the accuracy of MLP was slightly higher than RBF, however, both models were acceptable. Due to the high and acceptable accuracy of these two models, they can be well used in future research and applications. In this research, the main innovation is comparing two different methods for modelling the heat exchanger with a rectangular helical channel. This research shows that the use of perceptron neural network and radial basis function can both be effective in improving the performance and efficiency of the heat exchanger. This research can be used as a guide to choose the appropriate method for modeling heat exchangers and help to improve technologies related to this field&lt;/span&gt;.</Abstract>
			<OtherAbstract Language="FA">&lt;span style=&quot;letter-spacing: .05pt;&quot;&gt;In this research, computational fluid dynamics method was used to investigate the effect of geometrical parameters of rectangular spiral channels on heat transfer coefficient. Two artificial neural networks including perceptron (MLP) and radial basis function (RBF) models were used to model the heat transfer in helical channels. The model inputs included the Reynolds number and geometric parameters of the channels, and output was the Nusselt number. 135 data were generated by Computational Fluid Dynamics (CFD) simulation and after validation were used for training and evaluation of neural network models. The results of the research showed that the accuracy of MLP was slightly higher than RBF, however, both models were acceptable. Due to the high and acceptable accuracy of these two models, they can be well used in future research and applications. In this research, the main innovation is comparing two different methods for modelling the heat exchanger with a rectangular helical channel. This research shows that the use of perceptron neural network and radial basis function can both be effective in improving the performance and efficiency of the heat exchanger. This research can be used as a guide to choose the appropriate method for modeling heat exchangers and help to improve technologies related to this field&lt;/span&gt;.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Rectangular Spiral Channels</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Perceptron neural network</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Radial basis function</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">computational fluid dynamics</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">heat exchanger</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_5561_5cb22b6ada9b860235e5e20975f23de3.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>56</Volume>
				<Issue>5</Issue>
				<PubDate PubStatus="epublish">
					<Year>2024</Year>
					<Month>07</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Development of a novel multi-cellular origami metastructure and investigation into numerical and experimental energy absorption behaviour</ArticleTitle>
<VernacularTitle>Development of a novel multi-cellular origami metastructure and investigation into numerical and experimental energy absorption behaviour</VernacularTitle>
			<FirstPage>717</FirstPage>
			<LastPage>740</LastPage>
			<ELocationID EIdType="pii">5562</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2024.22928.7694</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Mohammad</FirstName>
					<LastName>Mazaheri</LastName>
<Affiliation>K. N. Toosi University of Technology</Affiliation>

</Author>
<Author>
					<FirstName>Mohammad</FirstName>
					<LastName>Khalajzadeh</LastName>
<Affiliation>K. N. Toosi University of technology</Affiliation>

</Author>
<Author>
					<FirstName>Masood</FirstName>
					<LastName>Asgari</LastName>
<Affiliation>هیات علمی</Affiliation>
<Identifier Source="ORCID">0000-0002-2063-8699</Identifier>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2024</Year>
					<Month>01</Month>
					<Day>16</Day>
				</PubDate>
			</History>
		<Abstract>Nowadays, the use of additive manufacturing provides a unique opportunity to create complex structures. One such structure that is currently garnering attention in various fields, such as energy absorption, is origami structures. In this paper, novel multi-cellular origami structures are introduced to improve energy absorption performance under quasi-static compression loading. The control of these structures is determined by two key parameters: the number of layers and the ratio between the length of the top side and the bottom side. The effects of these structures on crashworthiness were simulated using Abaqus software and validated through experimental tests with models built using additive manufacturing. Additionally, a simple structure was designed and tested to facilitate a comparison between origami and non-origami structures. The results of this study showed that geometric parameters play an important role in increasing energy absorption behaviour, with origami structures exhibiting a 97 percent increase in specific energy absorption (SEA) compared to non-origami structures. Finally, based on the complex proportional assessment method, the best structure was determined among those designed according to energy absorption criteria.</Abstract>
			<OtherAbstract Language="FA">Nowadays, the use of additive manufacturing provides a unique opportunity to create complex structures. One such structure that is currently garnering attention in various fields, such as energy absorption, is origami structures. In this paper, novel multi-cellular origami structures are introduced to improve energy absorption performance under quasi-static compression loading. The control of these structures is determined by two key parameters: the number of layers and the ratio between the length of the top side and the bottom side. The effects of these structures on crashworthiness were simulated using Abaqus software and validated through experimental tests with models built using additive manufacturing. Additionally, a simple structure was designed and tested to facilitate a comparison between origami and non-origami structures. The results of this study showed that geometric parameters play an important role in increasing energy absorption behaviour, with origami structures exhibiting a 97 percent increase in specific energy absorption (SEA) compared to non-origami structures. Finally, based on the complex proportional assessment method, the best structure was determined among those designed according to energy absorption criteria.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Origami</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Origami structures</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Energy Absorption</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Additive Manufacturing</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Multicellular origami metastructure</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_5562_e84401ad27c4cfb9815776eb9432ff17.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>56</Volume>
				<Issue>5</Issue>
				<PubDate PubStatus="epublish">
					<Year>2024</Year>
					<Month>07</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Experimental Study of Nano-Oils Containing Iron Oxide, multi-walled carbon nanotubes, and Aluminum Oxide in Reducing the Hot Spot Temperature of Transformers</ArticleTitle>
<VernacularTitle>Experimental Study of Nano-Oils Containing Iron Oxide, multi-walled carbon nanotubes, and Aluminum Oxide in Reducing the Hot Spot Temperature of Transformers</VernacularTitle>
			<FirstPage>741</FirstPage>
			<LastPage>762</LastPage>
			<ELocationID EIdType="pii">5566</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2024.22976.7702</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Fateme</FirstName>
					<LastName>Tavakoli Dastjerd</LastName>
<Affiliation>Department of Mechanical Engineering, Faculty of Engineering, Ferdowsi University of Mashhad, Mashhad, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Amirhossein</FirstName>
					<LastName>Joveini</LastName>
<Affiliation>Department of Mechanical Engineering, Faculty of Engineering, Ferdowsi University of Mashhad, Mashhad, Iran</Affiliation>
<Identifier Source="ORCID">0009-0004-2807-5044</Identifier>

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

</Author>
<Author>
					<FirstName>Hamid</FirstName>
					<LastName>Niazmand</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>02</Month>
					<Day>09</Day>
				</PubDate>
			</History>
		<Abstract>&lt;span style=&quot;letter-spacing: .05pt;&quot;&gt;In tropical regions, particularly during the summer, the rise in ambient temperature causes a significant increase in the hot spot temperature of transformers, which can result in the early failure of transformers and cause irreparable damage to the power grid. Therefore, efforts to reduce the hot spot temperature of transformers are of great importance. One method of thermal management for oil-immersed transformers is to enhance the heat transfer properties of the oil with additives, allowing for the effective and rapid dissipation of heat from the windings and core to the surrounding environment. In this study, the experimental performance of three nan-oil aluminium oxide, iron oxide, and multi-walled carbon nanotubes was evaluated in a laboratory-scale oil-immersed transformer with a maximum rated power of 150 watts. To this end, the aforementioned nanoparticles were mixed with transformer mineral oil at a concentration of 0.5 g/L and tested in the transformer. The results showed that adding nanoparticles to the oil, within the permissible range for various parameters, improved the physical properties of the nano-oil, which could play a significant role in the thermal management of transformer oil. For example, at 100% of the transformer&#039;s full power, the aluminium oxide, iron oxide, and multi-walled carbon nanotube nano-oils reduced the hot spot temperature by 2.1°C, 1.3°C, and 5.4°C, respectively, compared to the baseline test with mineral oil. The primary reason for this improvement is the enhanced thermal conductivity of the nano-oil.&lt;/span&gt;</Abstract>
			<OtherAbstract Language="FA">&lt;span style=&quot;letter-spacing: .05pt;&quot;&gt;In tropical regions, particularly during the summer, the rise in ambient temperature causes a significant increase in the hot spot temperature of transformers, which can result in the early failure of transformers and cause irreparable damage to the power grid. Therefore, efforts to reduce the hot spot temperature of transformers are of great importance. One method of thermal management for oil-immersed transformers is to enhance the heat transfer properties of the oil with additives, allowing for the effective and rapid dissipation of heat from the windings and core to the surrounding environment. In this study, the experimental performance of three nan-oil aluminium oxide, iron oxide, and multi-walled carbon nanotubes was evaluated in a laboratory-scale oil-immersed transformer with a maximum rated power of 150 watts. To this end, the aforementioned nanoparticles were mixed with transformer mineral oil at a concentration of 0.5 g/L and tested in the transformer. The results showed that adding nanoparticles to the oil, within the permissible range for various parameters, improved the physical properties of the nano-oil, which could play a significant role in the thermal management of transformer oil. For example, at 100% of the transformer&#039;s full power, the aluminium oxide, iron oxide, and multi-walled carbon nanotube nano-oils reduced the hot spot temperature by 2.1°C, 1.3°C, and 5.4°C, respectively, compared to the baseline test with mineral oil. The primary reason for this improvement is the enhanced thermal conductivity of the nano-oil.&lt;/span&gt;</OtherAbstract>
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			<Param Name="value">Nanoparticle</Param>
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			<Param Name="value">Hot Spot Temperature</Param>
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