Development and Numerical Justification of the Specimen for the Surface Crack Growth Rate Tests
In this work, based on the numerical analysis of the stress-strain state, the specimen for the surface crack growth rate tests at normal and elevated temperatures is developed. The known test methods for the surface crack growth rate determining are analyzed and the requirements for the specimen are...
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Veröffentlicht in: | Russian aeronautics 2022, Vol.65 (1), p.41-48 |
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creator | Yakovlev, M. M. Yarullin, R. R. Zakharov, A. P. |
description | In this work, based on the numerical analysis of the stress-strain state, the specimen for the surface crack growth rate tests at normal and elevated temperatures is developed. The known test methods for the surface crack growth rate determining are analyzed and the requirements for the specimen are formulated. |
doi_str_mv | 10.3103/S1068799822010056 |
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M. ; Yarullin, R. R. ; Zakharov, A. P.</creator><creatorcontrib>Yakovlev, M. M. ; Yarullin, R. R. ; Zakharov, A. P.</creatorcontrib><description>In this work, based on the numerical analysis of the stress-strain state, the specimen for the surface crack growth rate tests at normal and elevated temperatures is developed. The known test methods for the surface crack growth rate determining are analyzed and the requirements for the specimen are formulated.</description><identifier>ISSN: 1068-7998</identifier><identifier>EISSN: 1934-7901</identifier><identifier>DOI: 10.3103/S1068799822010056</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Automotive Engineering ; Crack propagation ; Engineering ; High temperature ; Numerical analysis ; Structural Mechanics and Strength of Flight Vehicles ; Surface cracks</subject><ispartof>Russian aeronautics, 2022, Vol.65 (1), p.41-48</ispartof><rights>Allerton Press, Inc. 2022</rights><rights>Allerton Press, Inc. 2022.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c1136-ef1ffa0084873cf2fc3bc6776ae5e1ad076908838b395177db0530340ddc7a0f3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.3103/S1068799822010056$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.3103/S1068799822010056$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,41464,42533,51294</link.rule.ids></links><search><creatorcontrib>Yakovlev, M. M.</creatorcontrib><creatorcontrib>Yarullin, R. R.</creatorcontrib><creatorcontrib>Zakharov, A. P.</creatorcontrib><title>Development and Numerical Justification of the Specimen for the Surface Crack Growth Rate Tests</title><title>Russian aeronautics</title><addtitle>Russ. Aeronaut</addtitle><description>In this work, based on the numerical analysis of the stress-strain state, the specimen for the surface crack growth rate tests at normal and elevated temperatures is developed. The known test methods for the surface crack growth rate determining are analyzed and the requirements for the specimen are formulated.</description><subject>Automotive Engineering</subject><subject>Crack propagation</subject><subject>Engineering</subject><subject>High temperature</subject><subject>Numerical analysis</subject><subject>Structural Mechanics and Strength of Flight Vehicles</subject><subject>Surface cracks</subject><issn>1068-7998</issn><issn>1934-7901</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp1kEFLAzEQhYMoWKs_wFvA8-ok2U2yR6laFVGw9byk2Ynd2m5qsqv4701ZwYN4mmHme-_BI-SUwblgIC5mDKRWZak5BwZQyD0yYqXIM1UC2097eme7_yE5inG1I3jOR6S6wg9c--0G246atqaP_QZDY82a3vexa1xau8a31DvaLZHOtmibBFPnw3DogzMW6SQY-0anwX92S_psOqRzjF08JgfOrCOe_Mwxebm5nk9us4en6d3k8iGzjAmZoWPOGQCdayWs486KhZVKSYMFMlODkiVoLfRClAVTql5AIUDkUNdWGXBiTM4G323w731Krla-D22KrHiykZIpzRPFBsoGH2NAV21DszHhq2JQ7Xqs_vSYNHzQxMS2rxh-nf8XfQMWxHPx</recordid><startdate>2022</startdate><enddate>2022</enddate><creator>Yakovlev, M. M.</creator><creator>Yarullin, R. R.</creator><creator>Zakharov, A. P.</creator><general>Pleiades Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>2022</creationdate><title>Development and Numerical Justification of the Specimen for the Surface Crack Growth Rate Tests</title><author>Yakovlev, M. M. ; Yarullin, R. R. ; Zakharov, A. P.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c1136-ef1ffa0084873cf2fc3bc6776ae5e1ad076908838b395177db0530340ddc7a0f3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Automotive Engineering</topic><topic>Crack propagation</topic><topic>Engineering</topic><topic>High temperature</topic><topic>Numerical analysis</topic><topic>Structural Mechanics and Strength of Flight Vehicles</topic><topic>Surface cracks</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Yakovlev, M. M.</creatorcontrib><creatorcontrib>Yarullin, R. R.</creatorcontrib><creatorcontrib>Zakharov, A. P.</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Russian aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Yakovlev, M. M.</au><au>Yarullin, R. R.</au><au>Zakharov, A. P.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Development and Numerical Justification of the Specimen for the Surface Crack Growth Rate Tests</atitle><jtitle>Russian aeronautics</jtitle><stitle>Russ. Aeronaut</stitle><date>2022</date><risdate>2022</risdate><volume>65</volume><issue>1</issue><spage>41</spage><epage>48</epage><pages>41-48</pages><issn>1068-7998</issn><eissn>1934-7901</eissn><abstract>In this work, based on the numerical analysis of the stress-strain state, the specimen for the surface crack growth rate tests at normal and elevated temperatures is developed. The known test methods for the surface crack growth rate determining are analyzed and the requirements for the specimen are formulated.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.3103/S1068799822010056</doi><tpages>8</tpages></addata></record> |
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subjects | Automotive Engineering Crack propagation Engineering High temperature Numerical analysis Structural Mechanics and Strength of Flight Vehicles Surface cracks |
title | Development and Numerical Justification of the Specimen for the Surface Crack Growth Rate Tests |
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