Study of Tensile Strength Distribution Based on Composite Materials for Aeronautical Engineering
The Tensile strength of an composite materials for aeronautical engineering was tested and its distribution was analyzed based on the two parameter weibull distribution. The maximum normed residual (MNR) test was applied to eliminate abnormal data. A graphical method was used to estimate parameters....
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Veröffentlicht in: | Modern applied science 2012-05, Vol.6 (5), p.21-21 |
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creator | Du, Baojiang Ji, Changqin Chen, Ping Guo, Jingmin Sun, Anbo Wei, Xiong |
description | The Tensile strength of an composite materials for aeronautical engineering was tested and its distribution was analyzed based on the two parameter weibull distribution. The maximum normed residual (MNR) test was applied to eliminate abnormal data. A graphical method was used to estimate parameters. Furthermore the validity of the assumed distribution was examined by the kolmogorov test (KS). The results show that MNR test can be used to exclude abnormal data. It also suggests that the gained two parameter weibull distribution can be used to express the tensile strength and predict its values accurately. |
doi_str_mv | 10.5539/mas.v6n5p21 |
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The maximum normed residual (MNR) test was applied to eliminate abnormal data. A graphical method was used to estimate parameters. Furthermore the validity of the assumed distribution was examined by the kolmogorov test (KS). The results show that MNR test can be used to exclude abnormal data. It also suggests that the gained two parameter weibull distribution can be used to express the tensile strength and predict its values accurately.</description><identifier>ISSN: 1913-1844</identifier><identifier>EISSN: 1913-1852</identifier><identifier>DOI: 10.5539/mas.v6n5p21</identifier><language>eng</language><subject>Aeronautical engineering ; Composite materials ; Estimates ; Graphical methods ; Tensile strength ; Weibull distribution</subject><ispartof>Modern applied science, 2012-05, Vol.6 (5), p.21-21</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c214t-681f46cecc0da720112f6f5f478fb620c3abfbc85bef7436c989f20de845cc763</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><creatorcontrib>Du, Baojiang</creatorcontrib><creatorcontrib>Ji, Changqin</creatorcontrib><creatorcontrib>Chen, Ping</creatorcontrib><creatorcontrib>Guo, Jingmin</creatorcontrib><creatorcontrib>Sun, Anbo</creatorcontrib><creatorcontrib>Wei, Xiong</creatorcontrib><title>Study of Tensile Strength Distribution Based on Composite Materials for Aeronautical Engineering</title><title>Modern applied science</title><description>The Tensile strength of an composite materials for aeronautical engineering was tested and its distribution was analyzed based on the two parameter weibull distribution. 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It also suggests that the gained two parameter weibull distribution can be used to express the tensile strength and predict its values accurately.</description><subject>Aeronautical engineering</subject><subject>Composite materials</subject><subject>Estimates</subject><subject>Graphical methods</subject><subject>Tensile strength</subject><subject>Weibull distribution</subject><issn>1913-1844</issn><issn>1913-1852</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2012</creationdate><recordtype>article</recordtype><recordid>eNqFkLtOwzAARS0EEqUw8QMekVCK30nGUspDKmJomYPj2MUosYPtIPXvSdWKlele6R7d4QBwjdGMc1redTLOfoTjPcEnYIJLTDNccHL61xk7BxcxfiEkSEnLCfhYp6HZQW_gRrtoWw3XKWi3TZ_wwcYUbD0k6x28l1E3cCwL3_U-2qThq0w6WNlGaHyAcx28kyOsZAuXbmudHle3vQRnZmT01TGn4P1xuVk8Z6u3p5fFfJUpglnKRIENE0orhRqZE4QxMcJww_LC1IIgRWVtalXwWpucUaHKojQENbpgXKlc0Cm4Ofz2wX8POqaqs1HptpVO-yFWOOeUlSLn7H-UEFzkhLE9entAVfAxBm2qPthOhl2FUbVXXo3Kq6Ny-gt3nHbP</recordid><startdate>201205</startdate><enddate>201205</enddate><creator>Du, Baojiang</creator><creator>Ji, Changqin</creator><creator>Chen, Ping</creator><creator>Guo, Jingmin</creator><creator>Sun, Anbo</creator><creator>Wei, Xiong</creator><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>201205</creationdate><title>Study of Tensile Strength Distribution Based on Composite Materials for Aeronautical Engineering</title><author>Du, Baojiang ; Ji, Changqin ; Chen, Ping ; Guo, Jingmin ; Sun, Anbo ; Wei, Xiong</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c214t-681f46cecc0da720112f6f5f478fb620c3abfbc85bef7436c989f20de845cc763</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2012</creationdate><topic>Aeronautical engineering</topic><topic>Composite materials</topic><topic>Estimates</topic><topic>Graphical methods</topic><topic>Tensile strength</topic><topic>Weibull distribution</topic><toplevel>online_resources</toplevel><creatorcontrib>Du, Baojiang</creatorcontrib><creatorcontrib>Ji, Changqin</creatorcontrib><creatorcontrib>Chen, Ping</creatorcontrib><creatorcontrib>Guo, Jingmin</creatorcontrib><creatorcontrib>Sun, Anbo</creatorcontrib><creatorcontrib>Wei, Xiong</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Modern applied science</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Du, Baojiang</au><au>Ji, Changqin</au><au>Chen, Ping</au><au>Guo, Jingmin</au><au>Sun, Anbo</au><au>Wei, Xiong</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Study of Tensile Strength Distribution Based on Composite Materials for Aeronautical Engineering</atitle><jtitle>Modern applied science</jtitle><date>2012-05</date><risdate>2012</risdate><volume>6</volume><issue>5</issue><spage>21</spage><epage>21</epage><pages>21-21</pages><issn>1913-1844</issn><eissn>1913-1852</eissn><abstract>The Tensile strength of an composite materials for aeronautical engineering was tested and its distribution was analyzed based on the two parameter weibull distribution. 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subjects | Aeronautical engineering Composite materials Estimates Graphical methods Tensile strength Weibull distribution |
title | Study of Tensile Strength Distribution Based on Composite Materials for Aeronautical Engineering |
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