Analysis of Vibration Characteristics for Rotating Braided Fiber-Reinforced Composite Annular Plates with Perforations
In the current study, a comprehensive numerical model for analyzing the vibrational characteristics of braided fiber-reinforced composite (BFRC) rotating annular plate with perforations under diverse boundary constraints was introduced. This model employs the differential quadrature finite element m...
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| Veröffentlicht in: | Materials 2024-11, Vol.17 (22), p.5402 |
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| description | In the current study, a comprehensive numerical model for analyzing the vibrational characteristics of braided fiber-reinforced composite (BFRC) rotating annular plate with perforations under diverse boundary constraints was introduced. This model employs the differential quadrature finite element method (DQFEM), which was developed based on the first-order shear deformation theory (FSDT) and coordinate transformation approach. The BFRC material, specifically a two-dimensional biaxial orthogonal fabric, was utilized to fabricate the annular plate with two distinct types of holes: circular and sector-shaped. The model's convergence, accuracy, numerical stability, and reliability were confirmed through comparative assessments utilizing data from the literature, from ABAQUS software, and from experimental findings. The analysis focuses on studying the influences of structural properties, material parameters, and boundary restraints on the frequencies of vibration for BFRC rotating annular plates with holes. This theoretical model helps provide scientific basis and technical guidance for the stability and lightweight design of rotating annular plates, such as rotor structures in aircraft engines. |
| doi_str_mv | 10.3390/ma17225402 |
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This model employs the differential quadrature finite element method (DQFEM), which was developed based on the first-order shear deformation theory (FSDT) and coordinate transformation approach. The BFRC material, specifically a two-dimensional biaxial orthogonal fabric, was utilized to fabricate the annular plate with two distinct types of holes: circular and sector-shaped. The model's convergence, accuracy, numerical stability, and reliability were confirmed through comparative assessments utilizing data from the literature, from ABAQUS software, and from experimental findings. The analysis focuses on studying the influences of structural properties, material parameters, and boundary restraints on the frequencies of vibration for BFRC rotating annular plates with holes. This theoretical model helps provide scientific basis and technical guidance for the stability and lightweight design of rotating annular plates, such as rotor structures in aircraft engines.</description><identifier>ISSN: 1996-1944</identifier><identifier>EISSN: 1996-1944</identifier><identifier>DOI: 10.3390/ma17225402</identifier><identifier>PMID: 39597225</identifier><language>eng</language><publisher>Switzerland: MDPI AG</publisher><subject>Aircraft engines ; Aircraft guidance ; Aircraft vibration ; Annular plates ; Boundary conditions ; Braided composites ; Braiding ; Composite materials ; Coordinate transformations ; Deformation ; Energy ; Fiber composites ; Finite element analysis ; Finite element method ; Investigations ; Mathematical analysis ; Mathematical models ; Numerical models ; Numerical stability ; Quadratures ; Rotation ; Shear deformation ; Shear strain ; Software reliability ; Stability ; Vibration analysis</subject><ispartof>Materials, 2024-11, Vol.17 (22), p.5402</ispartof><rights>COPYRIGHT 2024 MDPI AG</rights><rights>2024 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><rights>2024 by the authors. 2024</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c335t-dbde2b362b0cb80203b78bcc58ef6450471bc68858199123b2276326c0b871ff3</cites><orcidid>0000-0002-4557-9349</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.ncbi.nlm.nih.gov/pmc/articles/PMC11595680/pdf/$$EPDF$$P50$$Gpubmedcentral$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.ncbi.nlm.nih.gov/pmc/articles/PMC11595680/$$EHTML$$P50$$Gpubmedcentral$$Hfree_for_read</linktohtml><link.rule.ids>230,314,723,776,780,881,27901,27902,53766,53768</link.rule.ids><backlink>$$Uhttps://www.ncbi.nlm.nih.gov/pubmed/39597225$$D View this record in MEDLINE/PubMed$$Hfree_for_read</backlink></links><search><creatorcontrib>Zhang, Haibiao</creatorcontrib><creatorcontrib>Li, Zhen</creatorcontrib><creatorcontrib>Wang, Shixun</creatorcontrib><creatorcontrib>Liu, Tao</creatorcontrib><creatorcontrib>Wang, Qingshan</creatorcontrib><title>Analysis of Vibration Characteristics for Rotating Braided Fiber-Reinforced Composite Annular Plates with Perforations</title><title>Materials</title><addtitle>Materials (Basel)</addtitle><description>In the current study, a comprehensive numerical model for analyzing the vibrational characteristics of braided fiber-reinforced composite (BFRC) rotating annular plate with perforations under diverse boundary constraints was introduced. This model employs the differential quadrature finite element method (DQFEM), which was developed based on the first-order shear deformation theory (FSDT) and coordinate transformation approach. The BFRC material, specifically a two-dimensional biaxial orthogonal fabric, was utilized to fabricate the annular plate with two distinct types of holes: circular and sector-shaped. The model's convergence, accuracy, numerical stability, and reliability were confirmed through comparative assessments utilizing data from the literature, from ABAQUS software, and from experimental findings. The analysis focuses on studying the influences of structural properties, material parameters, and boundary restraints on the frequencies of vibration for BFRC rotating annular plates with holes. This theoretical model helps provide scientific basis and technical guidance for the stability and lightweight design of rotating annular plates, such as rotor structures in aircraft engines.</description><subject>Aircraft engines</subject><subject>Aircraft guidance</subject><subject>Aircraft vibration</subject><subject>Annular plates</subject><subject>Boundary conditions</subject><subject>Braided composites</subject><subject>Braiding</subject><subject>Composite materials</subject><subject>Coordinate transformations</subject><subject>Deformation</subject><subject>Energy</subject><subject>Fiber composites</subject><subject>Finite element analysis</subject><subject>Finite element method</subject><subject>Investigations</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Numerical models</subject><subject>Numerical stability</subject><subject>Quadratures</subject><subject>Rotation</subject><subject>Shear deformation</subject><subject>Shear strain</subject><subject>Software reliability</subject><subject>Stability</subject><subject>Vibration analysis</subject><issn>1996-1944</issn><issn>1996-1944</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNpdkl1vFCEUhomxsU3tjT_AkHhjTKbyMcwwV2a7adWkiU2j3hJgzuzSzMAKTE3_fdlOrVW4gJzznJfzAUJvKDnlvCMfJ01bxkRN2At0RLuuqWhX1y-f3Q_RSUo3pCzOqWTdK3TIO9Hto47Q7crr8S65hMOAfzoTdXbB4_VWR20zRJeyswkPIeLrkIvTb_BZ1K6HHl84A7G6BueL2xbDOky7kFwGvPJ-HnXEV6POkPBvl7f4CmLhHvTTa3Qw6DHByeN5jH5cnH9ff6kuv33-ul5dVpZzkave9MAMb5gh1kjCCDetNNYKCUNTC1K31NhGSiFLtZRxw1jbcNZYYmRLh4Efo0-L7m42E_QWfI56VLvoJh3vVNBO_evxbqs24VZRKjrRSFIU3j8qxPBrhpTV5JKFcdQewpwUp5zXQspGFPTdf-hNmGPp70Lxuu5kW6jThdroEdS-d-VhW3YPk7PBw-CKfSWpLPNdMviwBNgYUoowPKVPidr_AfX3DxT47fOCn9A_E-f3NvCs_A</recordid><startdate>20241105</startdate><enddate>20241105</enddate><creator>Zhang, Haibiao</creator><creator>Li, Zhen</creator><creator>Wang, Shixun</creator><creator>Liu, Tao</creator><creator>Wang, Qingshan</creator><general>MDPI AG</general><general>MDPI</general><scope>NPM</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>KB.</scope><scope>PDBOC</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>7X8</scope><scope>5PM</scope><orcidid>https://orcid.org/0000-0002-4557-9349</orcidid></search><sort><creationdate>20241105</creationdate><title>Analysis of Vibration Characteristics for Rotating Braided Fiber-Reinforced Composite Annular Plates with Perforations</title><author>Zhang, Haibiao ; Li, Zhen ; Wang, Shixun ; Liu, Tao ; Wang, Qingshan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c335t-dbde2b362b0cb80203b78bcc58ef6450471bc68858199123b2276326c0b871ff3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Aircraft engines</topic><topic>Aircraft guidance</topic><topic>Aircraft vibration</topic><topic>Annular plates</topic><topic>Boundary conditions</topic><topic>Braided composites</topic><topic>Braiding</topic><topic>Composite materials</topic><topic>Coordinate transformations</topic><topic>Deformation</topic><topic>Energy</topic><topic>Fiber composites</topic><topic>Finite element analysis</topic><topic>Finite element method</topic><topic>Investigations</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Numerical models</topic><topic>Numerical stability</topic><topic>Quadratures</topic><topic>Rotation</topic><topic>Shear deformation</topic><topic>Shear strain</topic><topic>Software reliability</topic><topic>Stability</topic><topic>Vibration analysis</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhang, Haibiao</creatorcontrib><creatorcontrib>Li, Zhen</creatorcontrib><creatorcontrib>Wang, Shixun</creatorcontrib><creatorcontrib>Liu, Tao</creatorcontrib><creatorcontrib>Wang, Qingshan</creatorcontrib><collection>PubMed</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>Materials Research Database</collection><collection>Materials Science Database</collection><collection>Materials Science Collection</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>MEDLINE - Academic</collection><collection>PubMed Central (Full Participant titles)</collection><jtitle>Materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhang, Haibiao</au><au>Li, Zhen</au><au>Wang, Shixun</au><au>Liu, Tao</au><au>Wang, Qingshan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Analysis of Vibration Characteristics for Rotating Braided Fiber-Reinforced Composite Annular Plates with Perforations</atitle><jtitle>Materials</jtitle><addtitle>Materials (Basel)</addtitle><date>2024-11-05</date><risdate>2024</risdate><volume>17</volume><issue>22</issue><spage>5402</spage><pages>5402-</pages><issn>1996-1944</issn><eissn>1996-1944</eissn><abstract>In the current study, a comprehensive numerical model for analyzing the vibrational characteristics of braided fiber-reinforced composite (BFRC) rotating annular plate with perforations under diverse boundary constraints was introduced. This model employs the differential quadrature finite element method (DQFEM), which was developed based on the first-order shear deformation theory (FSDT) and coordinate transformation approach. The BFRC material, specifically a two-dimensional biaxial orthogonal fabric, was utilized to fabricate the annular plate with two distinct types of holes: circular and sector-shaped. The model's convergence, accuracy, numerical stability, and reliability were confirmed through comparative assessments utilizing data from the literature, from ABAQUS software, and from experimental findings. The analysis focuses on studying the influences of structural properties, material parameters, and boundary restraints on the frequencies of vibration for BFRC rotating annular plates with holes. 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| subjects | Aircraft engines Aircraft guidance Aircraft vibration Annular plates Boundary conditions Braided composites Braiding Composite materials Coordinate transformations Deformation Energy Fiber composites Finite element analysis Finite element method Investigations Mathematical analysis Mathematical models Numerical models Numerical stability Quadratures Rotation Shear deformation Shear strain Software reliability Stability Vibration analysis |
| title | Analysis of Vibration Characteristics for Rotating Braided Fiber-Reinforced Composite Annular Plates with Perforations |
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