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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>55</Volume>
				<Issue>3</Issue>
				<PubDate PubStatus="epublish">
					<Year>2023</Year>
					<Month>05</Month>
					<Day>22</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Numerical investigation of the influence of operating conditions on the performance of PEMFC powered Unmanned Aerial Vehicle (UAV): a statistical approach</ArticleTitle>
<VernacularTitle>Numerical investigation of the influence of operating conditions on the performance of PEMFC powered Unmanned Aerial Vehicle (UAV): a statistical approach</VernacularTitle>
			<FirstPage>407</FirstPage>
			<LastPage>430</LastPage>
			<ELocationID EIdType="pii">5125</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2023.21358.7437</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Amirhamzeh</FirstName>
					<LastName>Farajollahi</LastName>
<Affiliation>Department of  Engineering, Imam Ali University, Tehran, Iran</Affiliation>
<Identifier Source="ORCID">0000-0001-9201-1871</Identifier>

</Author>
<Author>
					<FirstName>Mohsen</FirstName>
					<LastName>Rostami</LastName>
<Affiliation>Imam Ali University</Affiliation>

</Author>
<Author>
					<FirstName>Mohammareza</FirstName>
					<LastName>Hasheminasab</LastName>
<Affiliation>department of mechanical engieering Amirkabir university of technology</Affiliation>

</Author>
<Author>
					<FirstName>Mojtaba</FirstName>
					<LastName>Lak</LastName>
<Affiliation>Imam Ali university</Affiliation>

</Author>
<Author>
					<FirstName>Afshin</FirstName>
					<LastName>Shojaian</LastName>
<Affiliation>Imam Ali University</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>05</Month>
					<Day>02</Day>
				</PubDate>
			</History>
		<Abstract>In this research, the effect of various operating conditions on the performance of an Unmanned Aerial Vehicle (UAV) with a PEMFC propulsion system is surveyed using a statistical approach, namely the Design of Experiment technique (DOE). Results indicate that increasing operating pressure improves the efficiency parameter for both the PEMFC and the system 3.5% and 14.5% respectively. Although increasing cathode stoichiometry augments the PEMFC efficiency, it plummets the system efficiency up to 30.6%. In addition, the influence of operating altitude on the PEMFC efficiency is negligible, while it causes a substantial decline in the system efficiency (more than 30%). As proved, at any desired operating altitude, maximum efficiency for the system obtains when the operating pressure and cathode stoichiometry are set at their maximum and minimum bound, respectively.</Abstract>
			<OtherAbstract Language="FA">In this research, the effect of various operating conditions on the performance of an Unmanned Aerial Vehicle (UAV) with a PEMFC propulsion system is surveyed using a statistical approach, namely the Design of Experiment technique (DOE). Results indicate that increasing operating pressure improves the efficiency parameter for both the PEMFC and the system 3.5% and 14.5% respectively. Although increasing cathode stoichiometry augments the PEMFC efficiency, it plummets the system efficiency up to 30.6%. In addition, the influence of operating altitude on the PEMFC efficiency is negligible, while it causes a substantial decline in the system efficiency (more than 30%). As proved, at any desired operating altitude, maximum efficiency for the system obtains when the operating pressure and cathode stoichiometry are set at their maximum and minimum bound, respectively.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">PEM fuel cell (PEMFC)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Unmanned Aerial Vehicle (UAV)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Operating altitude</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Design of Experiment (DOE)</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Response Surface Method (RSM)</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_5125_37f65c068b7723cd7809ee2d31d7861c.pdf</ArchiveCopySource>
</Article>
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