The influence of cross-sectional thickness on fatigue crack growth
For thin structures, fatigue crack growth rates may vary with the structure's thickness for a given stress intensity factor range. This effect is mainly due to the change in the nature of the plastic deformation when the plastic zone size becomes comparable with, or greater than, the cross‐sect...
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Veröffentlicht in: | Fatigue & fracture of engineering materials & structures 1999-05, Vol.22 (5), p.437-444 |
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creator | Guo, W. Wang, C. H. Rose, L. R. F. |
description | For thin structures, fatigue crack growth rates may vary with the structure's thickness for a given stress intensity factor range. This effect is mainly due to the change in the nature of the plastic deformation when the plastic zone size becomes comparable with, or greater than, the cross‐sectional thickness. Variations in the constraint affect both the crack tip plastic blunting behaviour as well as the fatigue crack closure level. Approximate expressions are constructed for the constraint factor based on asymptotic values and numerical results, which are shown to correlate well with finite element results. It is demonstrated that the present results not only permit predictions of the specimen thickness effects on fatigue crack propagation under spectrum loading, but also eliminate the need to determine the constraint factor by curve‐fitting crack growth data. |
doi_str_mv | 10.1046/j.1460-2695.1999.00176.x |
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H. ; Rose, L. R. F.</creator><creatorcontrib>Guo, W. ; Wang, C. H. ; Rose, L. R. F.</creatorcontrib><description>For thin structures, fatigue crack growth rates may vary with the structure's thickness for a given stress intensity factor range. This effect is mainly due to the change in the nature of the plastic deformation when the plastic zone size becomes comparable with, or greater than, the cross‐sectional thickness. Variations in the constraint affect both the crack tip plastic blunting behaviour as well as the fatigue crack closure level. Approximate expressions are constructed for the constraint factor based on asymptotic values and numerical results, which are shown to correlate well with finite element results. It is demonstrated that the present results not only permit predictions of the specimen thickness effects on fatigue crack propagation under spectrum loading, but also eliminate the need to determine the constraint factor by curve‐fitting crack growth data.</description><identifier>ISSN: 8756-758X</identifier><identifier>EISSN: 1460-2695</identifier><identifier>DOI: 10.1046/j.1460-2695.1999.00176.x</identifier><identifier>CODEN: FFESEY</identifier><language>eng</language><publisher>Oxford, UK: Blackwell Science Ltd</publisher><subject>Applied sciences ; constraint factor ; crack closure ; crack growth ; Exact sciences and technology ; Fatigue ; Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology ; Metals. 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H.</creatorcontrib><creatorcontrib>Rose, L. R. F.</creatorcontrib><title>The influence of cross-sectional thickness on fatigue crack growth</title><title>Fatigue & fracture of engineering materials & structures</title><addtitle>Fatigue & Fracture of Engineering Materials & Structures</addtitle><description>For thin structures, fatigue crack growth rates may vary with the structure's thickness for a given stress intensity factor range. This effect is mainly due to the change in the nature of the plastic deformation when the plastic zone size becomes comparable with, or greater than, the cross‐sectional thickness. Variations in the constraint affect both the crack tip plastic blunting behaviour as well as the fatigue crack closure level. Approximate expressions are constructed for the constraint factor based on asymptotic values and numerical results, which are shown to correlate well with finite element results. It is demonstrated that the present results not only permit predictions of the specimen thickness effects on fatigue crack propagation under spectrum loading, but also eliminate the need to determine the constraint factor by curve‐fitting crack growth data.</description><subject>Applied sciences</subject><subject>constraint factor</subject><subject>crack closure</subject><subject>crack growth</subject><subject>Exact sciences and technology</subject><subject>Fatigue</subject><subject>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</subject><subject>Metals. 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Metallurgy</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Guo, W.</creatorcontrib><creatorcontrib>Wang, C. H.</creatorcontrib><creatorcontrib>Rose, L. R. F.</creatorcontrib><collection>Istex</collection><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Fatigue & fracture of engineering materials & structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Guo, W.</au><au>Wang, C. H.</au><au>Rose, L. R. F.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>The influence of cross-sectional thickness on fatigue crack growth</atitle><jtitle>Fatigue & fracture of engineering materials & structures</jtitle><addtitle>Fatigue & Fracture of Engineering Materials & Structures</addtitle><date>1999-05</date><risdate>1999</risdate><volume>22</volume><issue>5</issue><spage>437</spage><epage>444</epage><pages>437-444</pages><issn>8756-758X</issn><eissn>1460-2695</eissn><coden>FFESEY</coden><abstract>For thin structures, fatigue crack growth rates may vary with the structure's thickness for a given stress intensity factor range. This effect is mainly due to the change in the nature of the plastic deformation when the plastic zone size becomes comparable with, or greater than, the cross‐sectional thickness. Variations in the constraint affect both the crack tip plastic blunting behaviour as well as the fatigue crack closure level. Approximate expressions are constructed for the constraint factor based on asymptotic values and numerical results, which are shown to correlate well with finite element results. It is demonstrated that the present results not only permit predictions of the specimen thickness effects on fatigue crack propagation under spectrum loading, but also eliminate the need to determine the constraint factor by curve‐fitting crack growth data.</abstract><cop>Oxford, UK</cop><pub>Blackwell Science Ltd</pub><doi>10.1046/j.1460-2695.1999.00176.x</doi><tpages>8</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Applied sciences constraint factor crack closure crack growth Exact sciences and technology Fatigue Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology Metals. Metallurgy |
title | The influence of cross-sectional thickness on fatigue crack growth |
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