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<ArticleSet>
<Article>
<Journal>
				<PublisherName>Sharif University of Technology</PublisherName>
				<JournalTitle>Scientia Iranica</JournalTitle>
				<Issn>1026-3098</Issn>
				<Volume>30</Volume>
				<Issue>4</Issue>
				<PubDate PubStatus="epublish">
					<Year>2023</Year>
					<Month>08</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>A new model for predicting fretting fatigue crack initiation life based on effective slip amplitude</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>1255</FirstPage>
			<LastPage>1264</LastPage>
			<ELocationID EIdType="pii">23041</ELocationID>
			
<ELocationID EIdType="doi">10.24200/sci.2022.60534.6849</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>E.</FirstName>
					<LastName>Badrikouhi</LastName>
<Affiliation>Department of Aerospace Engineering, Sharif University of Technology, 11365-11155, Tehran, Iran</Affiliation>
<Identifier Source="ORCID">0000-0002-0758-0488</Identifier>

</Author>
<Author>
					<FirstName>S.</FirstName>
					<LastName>Adibnazari</LastName>
<Affiliation>Department of Aerospace Engineering, Sharif University of Technology, 11365-11155, Tehran, Iran</Affiliation>
<Identifier Source="ORCID">0000-0002-0213-9589</Identifier>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>06</Month>
					<Day>01</Day>
				</PubDate>
			</History>
		<Abstract>In this study, a new model has been developed for fretting fatigue crack initiation life prediction based on the slip amplitude as a macroscopic feature of the contact interfaces. The main difference between the presented model and many other fretting fatigue life prediction models is the focus on the fretting specific characteristics. In this model, a damage parameter is combined with a damage severity factor to obtain a new fretting fatigue crack initiation life prediction parameter. To investigate the accuracy of this new parameter, a series of fretting fatigue tests have been conducted. Also, crack initiation life data from the literature were added to enhance parameter accuracy investigation. It is shown that the effective slip amplitude is an unbiased geometric-independent parameter in fretting fatigue crack initiation life prediction. Also, comparing prediction results from the effective slip amplitude with those of Smith-Watson-Topper and Ruiz parameters showed that the new parameter can outperform available fretting fatigue life prediction parameters.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Fretting Fatigue</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Slip Amplitude</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Life Prediction</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://scientiairanica.sharif.edu/article_23041_98465964ca8cd261e30c525aae7ba618.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Sharif University of Technology</PublisherName>
				<JournalTitle>Scientia Iranica</JournalTitle>
				<Issn>1026-3098</Issn>
				<Volume>30</Volume>
				<Issue>4</Issue>
				<PubDate PubStatus="epublish">
					<Year>2023</Year>
					<Month>08</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Vibration behavior of misaligned rotor with the asymmetric shaft using Timoshenko beam theory</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>1265</FirstPage>
			<LastPage>1278</LastPage>
			<ELocationID EIdType="pii">23066</ELocationID>
			
<ELocationID EIdType="doi">10.24200/sci.2022.57914.5473</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>H.</FirstName>
					<LastName>Jamshidi</LastName>
<Affiliation>Faculty Member of Mechanical Engineering, Parand Branch, Islamic Azad University, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>A. A.</FirstName>
					<LastName>Jafari</LastName>
<Affiliation>- Faculty Member of Mechanical Engineering, West Tehran Branch, Islamic Azad University, Tehran, Iran
- Faculty Member of Mechanical Engineering, K.N. Toosi University of Technology, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>P.</FirstName>
					<LastName>Jamshidi</LastName>
<Affiliation>Head of Turbo Compressor Maintenance Department at SPGC, Tehran, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2021</Year>
					<Month>03</Month>
					<Day>15</Day>
				</PubDate>
			</History>
		<Abstract>In the present study, an accurate model is used for analyzing an asymmetric shaft with misalignment and under unbalance forces in rotating coordinates verified by developing an experimental test.The asymmetric rotor modeled by the Timoshenko beam theory is coupled to a motor.The differential equations of motion are discretized by Rayleigh-Ritz method and derived from Hamilton&#039;s principle. Thereafter, According to the results, a frequency range is detected in which,resonance and instability will occur. The dynamic behavior of the rotor is investigated near the boundary of the instability region. Various parameters, including unbalanced and misalignment induced forces, and the dimensions of the cross-section of the shaft are taken into account.Finally,vibration responses of the system and their Fast Fourier Transform (FFT) are presented graphically to determine the frequencies of the harmonic responses. It is concluded that the asymmetry of the shaft and misalignment fault severely affect the dynamic response of the rotor.Moreover, the accuracy of the results is increased by applying the Timoshenko beam theory.By developing an experimental test for the rotor system connected to an electric motor with misalignment fault, verifying this model has been done.The experimental results obviously obtained the unstable operating area as acquired by the differential equations of motion.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Asymmetric Rotor</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Timoshenko Beam Theory</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Misalignment</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">mass unbalance</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Vibration</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://scientiairanica.sharif.edu/article_23066_dfadb3951b95acdd8571548ae4d6cf0d.pdf</ArchiveCopySource>
</Article>
</ArticleSet>
