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<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>57</Volume>
				<Issue>10</Issue>
				<PubDate PubStatus="epublish">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Thermal performance assessment of two side-by-side natural draft dry cooling towers with circular and elliptical periphery radiator arrangements</ArticleTitle>
<VernacularTitle>Thermal performance assessment of two side-by-side natural draft dry cooling towers with circular and elliptical periphery radiator arrangements</VernacularTitle>
			<FirstPage>1239</FirstPage>
			<LastPage>1262</LastPage>
			<ELocationID EIdType="pii">6021</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2026.25198.7927</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Yaser</FirstName>
					<LastName>Farahani</LastName>
<Affiliation>Faculty of Engineering, Bu-Ali Sina University, Hamedan, Iran</Affiliation>
<Identifier Source="ORCID">0009-0006-5461-3891</Identifier>

</Author>
<Author>
					<FirstName>Mohsen</FirstName>
					<LastName>Goodarzi</LastName>
<Affiliation>Faculty of Engineering, Bu-Ali Sina University, Hamedan, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>02</Day>
				</PubDate>
			</History>
		<Abstract>Wind significantly deteriorates thermal performance of natural draft dry cooling towers (NDDCTs). Although various approaches have been proposed to enhance the performance of single and multiple cooling towers, the effect of modifying the geometric arrangement of the radiators has not been comprehensively investigated. In this study, the thermal performance of two side-by-side natural draft dry cooling towers with an elliptical radiator arrangement was numerically compared with that of a conventional circular arrangement using three-dimensional CFD simulations. Results revealed that the presence of an adjacent tower leads to a reduction in the heat transfer rate of each individual tower compared to the isolated (single-tower) condition, highlighting the significant impact of flow interference between the towers. However, at wind speeds of 7 and 10 m/s, the elliptical arrangement outperformed the circular layout. Under high-wind conditions, the elliptical tower improves the thermal efficiency by approximately 18.2% to 29.5% compared to the conventional circular tower. Detailed flow field analysis revealed that the enhanced passage of warm air over the rear radiators in the elliptical arrangement increased the average temperature gradient along the lateral surfaces of these radiators, thereby improving their heat transfer rate. The optimal radiator arrangement depends on the prevailing wind conditions at the site and plays a critical role in improving the thermal performance of the cooling towers.</Abstract>
			<OtherAbstract Language="FA">Wind significantly deteriorates thermal performance of natural draft dry cooling towers (NDDCTs). Although various approaches have been proposed to enhance the performance of single and multiple cooling towers, the effect of modifying the geometric arrangement of the radiators has not been comprehensively investigated. In this study, the thermal performance of two side-by-side natural draft dry cooling towers with an elliptical radiator arrangement was numerically compared with that of a conventional circular arrangement using three-dimensional CFD simulations. Results revealed that the presence of an adjacent tower leads to a reduction in the heat transfer rate of each individual tower compared to the isolated (single-tower) condition, highlighting the significant impact of flow interference between the towers. However, at wind speeds of 7 and 10 m/s, the elliptical arrangement outperformed the circular layout. Under high-wind conditions, the elliptical tower improves the thermal efficiency by approximately 18.2% to 29.5% compared to the conventional circular tower. Detailed flow field analysis revealed that the enhanced passage of warm air over the rear radiators in the elliptical arrangement increased the average temperature gradient along the lateral surfaces of these radiators, thereby improving their heat transfer rate. The optimal radiator arrangement depends on the prevailing wind conditions at the site and plays a critical role in improving the thermal performance of the cooling towers.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Natural draft dry cooling tower</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Elliptical cooling tower</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Circular cooling tower</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Windy condition</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Side-by-side arrangement</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_6021_b075703bbe07a50ddcccfaac424bb6d9.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>57</Volume>
				<Issue>10</Issue>
				<PubDate PubStatus="epublish">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>A data-driven framework for wind turbine power curve cleaning and abnormal data detection based on binning and quantiles</ArticleTitle>
<VernacularTitle>A data-driven framework for wind turbine power curve cleaning and abnormal data detection based on binning and quantiles</VernacularTitle>
			<FirstPage>1263</FirstPage>
			<LastPage>1286</LastPage>
			<ELocationID EIdType="pii">6028</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2026.24688.7894</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Alireza</FirstName>
					<LastName>Aghajani Mobarakeh</LastName>
<Affiliation>Control Group, Department of Electrical Engineering, Iran University of Science and Technology, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Javad</FirstName>
					<LastName>Poshtan</LastName>
<Affiliation>Control Group, Department of Electrical Engineering, Iran University of Science and Technology, Tehran, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>09</Month>
					<Day>05</Day>
				</PubDate>
			</History>
		<Abstract>In this study, a preprocessing approach is proposed to improve training accuracy and computational efficiency by leveraging SCADA data and integrating machine learning algorithms with statistical techniques for unlabeled data. The method reduces the training dataset substantially by partitioning the data into equal points intervals and selecting representative samples based on quantiles, a procedure referred to as RD. Using this strategy, only 0.2% of the original dataset is required for model training in this study. Subsequently, abnormal data points are identified using a power curve model with quantile thresholds. The RD method is evaluated against DBSCAN and a KNN-based model. Experimental results obtained from real-world wind farm data indicate that RD combined with KNN outperforms DBSCAN. Specifically, both MAE and RMSE are reduced by approximately 15%, reflecting improved predictive accuracy. From a computational perspective, the execution time of RD is about 0.15 seconds, compared to 0.99 seconds for DBSCAN, corresponding to a reduction in runtime exceeding 50%. Moreover, unlike DBSCAN, which requires precise parameter tuning or additional constraints tailored to the power curve structure when dealing with dense or linear outliers, the proposed approach is capable of automatically eliminating outlier data points from the wind turbine power curve without the need for predefined filters or explicit boundary definitions prior to the cleaning process.</Abstract>
			<OtherAbstract Language="FA">In this study, a preprocessing approach is proposed to improve training accuracy and computational efficiency by leveraging SCADA data and integrating machine learning algorithms with statistical techniques for unlabeled data. The method reduces the training dataset substantially by partitioning the data into equal points intervals and selecting representative samples based on quantiles, a procedure referred to as RD. Using this strategy, only 0.2% of the original dataset is required for model training in this study. Subsequently, abnormal data points are identified using a power curve model with quantile thresholds. The RD method is evaluated against DBSCAN and a KNN-based model. Experimental results obtained from real-world wind farm data indicate that RD combined with KNN outperforms DBSCAN. Specifically, both MAE and RMSE are reduced by approximately 15%, reflecting improved predictive accuracy. From a computational perspective, the execution time of RD is about 0.15 seconds, compared to 0.99 seconds for DBSCAN, corresponding to a reduction in runtime exceeding 50%. Moreover, unlike DBSCAN, which requires precise parameter tuning or additional constraints tailored to the power curve structure when dealing with dense or linear outliers, the proposed approach is capable of automatically eliminating outlier data points from the wind turbine power curve without the need for predefined filters or explicit boundary definitions prior to the cleaning process.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Data Cleaning</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Wind Turbine Power Curve (WTPC)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">machine learning (ML)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Supervisory Control and Data Acquisition (SCADA)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Abnormal Detection (AD)</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_6028_2c60e40b399dc55d8b755ec6b5d09f8a.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>57</Volume>
				<Issue>10</Issue>
				<PubDate PubStatus="epublish">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Adjoint-Based Sensitivity Analysis of a Fixed Cross-Section Fin with Temperature-Dependent Conductivity</ArticleTitle>
<VernacularTitle>Adjoint-Based Sensitivity Analysis of a Fixed Cross-Section Fin with Temperature-Dependent Conductivity</VernacularTitle>
			<FirstPage>1287</FirstPage>
			<LastPage>1306</LastPage>
			<ELocationID EIdType="pii">6039</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2026.25461.7948</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Behzad</FirstName>
					<LastName>Baghapour</LastName>
<Affiliation>Mechanical Engineering Department, Amirkabir University of Technology, Iran</Affiliation>
<Identifier Source="ORCID">0000-0003-0235-0605</Identifier>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2026</Year>
					<Month>01</Month>
					<Day>29</Day>
				</PubDate>
			</History>
		<Abstract>In this paper, the sensitivity of the efficiency of a fixed cross-sectional fin with temperature-dependent thermal conductivity to various parameters is investigated using the adjoint equation. A one-dimensional steady-state formulation is assumed for both the governing energy equation and the corresponding adjoint equation. The appropriate boundary condition for a convective fin tip is derived for the adjoint variable. The energy and adjoint equations are solved numerically using a finite-difference scheme. The results indicate that a slight increase in certain parameters, such as the cross-sectional area and the base thermal conductivity, leads to an improvement in fin efficiency. In contrast, increasing parameters such as the fluid heat transfer coefficient and the fin length results in a reduction in efficiency. The slope factor in the linear thermal conductivity model exhibits a non-monotonic effect: for negative values, increasing the slope reduces fin efficiency, whereas for positive values, it enhances the efficiency. Furthermore, the Biot number defined along the fin length shows a pronounced negative influence on fin efficiency as it increases. Its most significant impact occurs around a Biot number of 0.1, corresponding to the transition from a nearly uniform temperature distribution to a regime with a pronounced internal temperature gradient.</Abstract>
			<OtherAbstract Language="FA">In this paper, the sensitivity of the efficiency of a fixed cross-sectional fin with temperature-dependent thermal conductivity to various parameters is investigated using the adjoint equation. A one-dimensional steady-state formulation is assumed for both the governing energy equation and the corresponding adjoint equation. The appropriate boundary condition for a convective fin tip is derived for the adjoint variable. The energy and adjoint equations are solved numerically using a finite-difference scheme. The results indicate that a slight increase in certain parameters, such as the cross-sectional area and the base thermal conductivity, leads to an improvement in fin efficiency. In contrast, increasing parameters such as the fluid heat transfer coefficient and the fin length results in a reduction in efficiency. The slope factor in the linear thermal conductivity model exhibits a non-monotonic effect: for negative values, increasing the slope reduces fin efficiency, whereas for positive values, it enhances the efficiency. Furthermore, the Biot number defined along the fin length shows a pronounced negative influence on fin efficiency as it increases. Its most significant impact occurs around a Biot number of 0.1, corresponding to the transition from a nearly uniform temperature distribution to a regime with a pronounced internal temperature gradient.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Sensitivity analysis</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">fin efficiency</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">temperature-dependent conductivity</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">adjoint equation</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">finite-difference method</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_6039_eb2e9dffe58d635b7d72e99c8e61b5f2.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>57</Volume>
				<Issue>10</Issue>
				<PubDate PubStatus="epublish">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Experimental Investigation of the Simultaneous Effect of Temperature and Aging on Mechanical Safety and Failure Behavior of Cylindrical Lithium-Ion Batteries Under Dynamic Impact</ArticleTitle>
<VernacularTitle>Experimental Investigation of the Simultaneous Effect of Temperature and Aging on Mechanical Safety and Failure Behavior of Cylindrical Lithium-Ion Batteries Under Dynamic Impact</VernacularTitle>
			<FirstPage>1307</FirstPage>
			<LastPage>1322</LastPage>
			<ELocationID EIdType="pii">6040</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2026.24433.7868</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Mohammad Ali</FirstName>
					<LastName>Ehteram</LastName>
<Affiliation>Mechanical and Energy Engineering, Shahid Beheshti University</Affiliation>

</Author>
<Author>
					<FirstName>Amir</FirstName>
					<LastName>Nezhadsafar</LastName>
<Affiliation>Faculty of Mechanical and Energy Engineering, Shahid Beheshti University</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>07</Month>
					<Day>21</Day>
				</PubDate>
			</History>
		<Abstract>The present research aims to experimentally evaluate the safety behavior and failure mechanism of 18650 cylindrical lithium-ion battery cells under dynamic impact loading. To this end, a pneumatic impact testing apparatus was developed in accordance with the SAE J2464 standard to assess the simultaneous effects of initial temperature (25, 0, and -25 °C), state of charge (10% and 100%), and state of health (fresh and aged over 400 cycles). Experimental results derived from high-speed imaging and thermal data analysis indicated that at ambient temperature, impact with a critical velocity of 9.23 m/s on fully charged samples led to immediate separator rupture and extensive internal short circuit. Under these conditions, the cell voltage dropped to zero within 290 ms, and explosive thermal runaway occurred with a severe temperature rise reaching 662 °C. In contrast, the most significant finding of this study reveals a substantial enhancement in the cell&#039;s mechanical resistance at sub-zero temperatures; remarkably, at -25 °C, no penetration or exothermic reaction was recorded even at high impact velocities. Further analysis suggests that the partial solidification and increased viscosity of the electrolyte at low temperatures act as an internal support with quasi-solid behavior, thereby preventing local stress concentration and separator tearing.</Abstract>
			<OtherAbstract Language="FA">The present research aims to experimentally evaluate the safety behavior and failure mechanism of 18650 cylindrical lithium-ion battery cells under dynamic impact loading. To this end, a pneumatic impact testing apparatus was developed in accordance with the SAE J2464 standard to assess the simultaneous effects of initial temperature (25, 0, and -25 °C), state of charge (10% and 100%), and state of health (fresh and aged over 400 cycles). Experimental results derived from high-speed imaging and thermal data analysis indicated that at ambient temperature, impact with a critical velocity of 9.23 m/s on fully charged samples led to immediate separator rupture and extensive internal short circuit. Under these conditions, the cell voltage dropped to zero within 290 ms, and explosive thermal runaway occurred with a severe temperature rise reaching 662 °C. In contrast, the most significant finding of this study reveals a substantial enhancement in the cell&#039;s mechanical resistance at sub-zero temperatures; remarkably, at -25 °C, no penetration or exothermic reaction was recorded even at high impact velocities. Further analysis suggests that the partial solidification and increased viscosity of the electrolyte at low temperatures act as an internal support with quasi-solid behavior, thereby preventing local stress concentration and separator tearing.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Lithium-ion Battery</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Safety</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Mechanical Impact</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">temperature effect</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Thermal Runaway</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_6040_4c9d1fbce4890fc2731b6a61262313b1.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>57</Volume>
				<Issue>10</Issue>
				<PubDate PubStatus="epublish">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Dynamic Sensitivity Analysis of a Free-Free Aluminum Beam Under Transient Multi-Point Impact Excitation Using Experimental Modal Analysis, Numerical Simulation, and Analytical Modeling</ArticleTitle>
<VernacularTitle>Dynamic Sensitivity Analysis of a Free-Free Aluminum Beam Under Transient Multi-Point Impact Excitation Using Experimental Modal Analysis, Numerical Simulation, and Analytical Modeling</VernacularTitle>
			<FirstPage>1323</FirstPage>
			<LastPage>1358</LastPage>
			<ELocationID EIdType="pii">6041</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2026.24330.7861</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Mehrdad</FirstName>
					<LastName>Karimi</LastName>
<Affiliation>Aerospace, Faculty of Postgraduate Studies, Shahid Sattari University, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Masoud</FirstName>
					<LastName>Javadi</LastName>
<Affiliation>Assistant Professor, Faculty of Aerospace, Shahid Sattari University, Tehran, Iran</Affiliation>
<Identifier Source="ORCID">0000-0003-0280-3643</Identifier>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>07</Month>
					<Day>08</Day>
				</PubDate>
			</History>
		<Abstract>Dynamic analysis plays a crucial role in predicting the vibrational behavior of structural systems. This study aims to accurately extract the modal characteristics of a free-free aluminum beam through a synergistic integration of experimental, analytical, and numerical approaches. In the experimental phase, calibrated modal hammer tests were conducted at six nodal positions, and the dynamic responses were captured using precision signal analyzers. The acquired data were processed in the specialized Star software using advanced signal processing algorithms to extract modal parameters with minimal systematic error. In the analytical phase, a mathematical model based on the governing differential equations of elastic structures—accounting for structural damping—was developed in MATLAB. Natural frequencies and mode shapes were identified using Peak Picking and Circle Fitting techniques. Additionally, finite element analysis was carried out in Abaqus, utilizing fine rectangular meshing and high-order hexahedral elements, which demonstrated excellent performance in simulating the system’s vibrational behavior under resonant conditions. Comparison of the results showed strong agreement in the frequency range of 0 to 1700 Hz, with deviations of less than 0.01% when considering the first mode as a rigid-body mode. This study highlights the importance of selecting appropriate excitation points to ensure accurate modal identification and confirms the proposed framework’s potential for analyzing more complex engineering structures.</Abstract>
			<OtherAbstract Language="FA">Dynamic analysis plays a crucial role in predicting the vibrational behavior of structural systems. This study aims to accurately extract the modal characteristics of a free-free aluminum beam through a synergistic integration of experimental, analytical, and numerical approaches. In the experimental phase, calibrated modal hammer tests were conducted at six nodal positions, and the dynamic responses were captured using precision signal analyzers. The acquired data were processed in the specialized Star software using advanced signal processing algorithms to extract modal parameters with minimal systematic error. In the analytical phase, a mathematical model based on the governing differential equations of elastic structures—accounting for structural damping—was developed in MATLAB. Natural frequencies and mode shapes were identified using Peak Picking and Circle Fitting techniques. Additionally, finite element analysis was carried out in Abaqus, utilizing fine rectangular meshing and high-order hexahedral elements, which demonstrated excellent performance in simulating the system’s vibrational behavior under resonant conditions. Comparison of the results showed strong agreement in the frequency range of 0 to 1700 Hz, with deviations of less than 0.01% when considering the first mode as a rigid-body mode. This study highlights the importance of selecting appropriate excitation points to ensure accurate modal identification and confirms the proposed framework’s potential for analyzing more complex engineering structures.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">modal analysis</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">impact excitation</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Natural frequency</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">frequency response matrix</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_6041_58ee2794cc87707943624dc8db2ff5a0.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>57</Volume>
				<Issue>10</Issue>
				<PubDate PubStatus="epublish">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Optimizing the Distance-to-Diameter Ratio in a Marine Ducted Propeller Using CFD and Genetic Algorithm, with Comparison to the KP505 Reference Propeller</ArticleTitle>
<VernacularTitle>Optimizing the Distance-to-Diameter Ratio in a Marine Ducted Propeller Using CFD and Genetic Algorithm, with Comparison to the KP505 Reference Propeller</VernacularTitle>
			<FirstPage>1359</FirstPage>
			<LastPage>1386</LastPage>
			<ELocationID EIdType="pii">6044</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2026.25245.7933</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>MohammadHasan</FirstName>
					<LastName>Ahmadi</LastName>
<Affiliation>Sea-Based Energy research group, Babol Noshirvani University of Technology</Affiliation>

</Author>
<Author>
					<FirstName>Rouzbeh</FirstName>
					<LastName>Shafaghat</LastName>
<Affiliation>Department of Mechanical Engineering, Babol Noshirvani University of Technology</Affiliation>

</Author>
<Author>
					<FirstName>Mohsen</FirstName>
					<LastName>Zamani</LastName>
<Affiliation>Sea-Based Energy research group, Babol Noshirvani University of Technology</Affiliation>

</Author>
<Author>
					<FirstName>Behrad</FirstName>
					<LastName>Alizadeh Kharkeshi</LastName>
<Affiliation>Faculty of Mechanical Engineering, Babol Noshirvani University of Technology</Affiliation>
<Identifier Source="ORCID">0000-0001-6522-6914</Identifier>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2025</Year>
					<Month>12</Month>
					<Day>09</Day>
				</PubDate>
			</History>
		<Abstract>Numerical simulations were performed using STAR-CCM+ software, and optimization was carried out with a genetic algorithm. The ducted propellers were innovatively designed based on the KP505 propeller. Simulations were conducted at six pitch ratios. To evaluate the results and perform optimization, thrust, torque, and efficiency coefficients were considered as objective functions. The results showed that the thrust coefficient exhibited a decreasing trend at low advance ratios, a non-linear behavior at medium advance ratios, and an increasing trend at high advance ratios as the pitch ratio increased. A comparative analysis revealed that before optimization, the ducted propeller&#039;s thrust coefficient was at best 15% higher than that of the KP505 propeller at an advance ratio of 0.8. The optimal pitch ratio obtained after optimization was 0.2641, corresponding to a maximum efficiency of 45.35% for the ducted propeller. Performance comparison between the optimized ducted propeller and the KP505 propeller showed that the optimized ducted propeller could increase thrust by up to 26% (at an advance ratio of 0.8) and improve efficiency by 7.84% at an advance ratio of 1.0. Flow analysis also indicated that increased velocity behind the propeller and an improved pressure pattern in the optimized ducted propeller contribute to higher thrust and reduced cavitation risk.</Abstract>
			<OtherAbstract Language="FA">Numerical simulations were performed using STAR-CCM+ software, and optimization was carried out with a genetic algorithm. The ducted propellers were innovatively designed based on the KP505 propeller. Simulations were conducted at six pitch ratios. To evaluate the results and perform optimization, thrust, torque, and efficiency coefficients were considered as objective functions. The results showed that the thrust coefficient exhibited a decreasing trend at low advance ratios, a non-linear behavior at medium advance ratios, and an increasing trend at high advance ratios as the pitch ratio increased. A comparative analysis revealed that before optimization, the ducted propeller&#039;s thrust coefficient was at best 15% higher than that of the KP505 propeller at an advance ratio of 0.8. The optimal pitch ratio obtained after optimization was 0.2641, corresponding to a maximum efficiency of 45.35% for the ducted propeller. Performance comparison between the optimized ducted propeller and the KP505 propeller showed that the optimized ducted propeller could increase thrust by up to 26% (at an advance ratio of 0.8) and improve efficiency by 7.84% at an advance ratio of 1.0. Flow analysis also indicated that increased velocity behind the propeller and an improved pressure pattern in the optimized ducted propeller contribute to higher thrust and reduced cavitation risk.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Numerical study</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Ducted propeller</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Pitch ratio</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">genetic algorithm</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">KP505 propeller</Param>
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