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Short crack threshold estimates to predict notch sensitivity factors in fatigue
The notch sensitivity factor q can be associated with the presence of non-propagating fatigue cracks at the notch root. Such cracks are present when the nominal stress range Δ σ n is between Δ σ 0/ K t and Δ σ 0/ K f, where Δ σ 0 is the fatigue limit, K t is the geometric and K f is the fatigue stre...
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Published in: | International journal of fatigue 2007-09, Vol.29 (9), p.2022-2031 |
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creator | Meggiolaro, Marco Antonio Miranda, Antonio Carlos de Oliveira de Castro, Jaime Tupiassú Pinho |
description | The notch sensitivity factor
q can be associated with the presence of non-propagating fatigue cracks at the notch root. Such cracks are present when the nominal stress range Δ
σ
n is between Δ
σ
0/
K
t and Δ
σ
0/
K
f, where Δ
σ
0 is the fatigue limit,
K
t is the geometric and
K
f is the fatigue stress concentration factors of the notch. Therefore, in principle it is possible to obtain expressions for
q if the propagation behavior of small cracks emanating from notches is known. Several expressions have been proposed to model the dependency between the threshold value Δ
K
th of the stress intensity range and the crack size
a for very small cracks. Most of these expressions are based on length parameters, estimated from Δ
K
th and Δ
σ
0, resulting in a modified stress intensity range able to reproduce most of the behavior shown in the Kitagawa–Takahashi plot. Peterson or Topper-like expressions are then calibrated to
q based on these crack propagation estimates. However, such
q calibration is found to be extremely sensitive to the choice of Δ
K
th(
a) estimate. In this work, a generalization version of El Haddad–Topper–Smith’s equation is used to evaluate the behavior of cracks emanating from circular holes and semi-elliptical notches. For several combinations of notch dimensions, the smallest stress range necessary to both initiate and propagate a crack is calculated, resulting in expressions for
K
f and therefore for
q. It is found that the
q estimates obtained from this generalization, besides providing a sound physical basis for the notch sensitivity concept, better correlate with experimental data from the literature. |
doi_str_mv | 10.1016/j.ijfatigue.2007.02.022 |
format | article |
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q can be associated with the presence of non-propagating fatigue cracks at the notch root. Such cracks are present when the nominal stress range Δ
σ
n is between Δ
σ
0/
K
t and Δ
σ
0/
K
f, where Δ
σ
0 is the fatigue limit,
K
t is the geometric and
K
f is the fatigue stress concentration factors of the notch. Therefore, in principle it is possible to obtain expressions for
q if the propagation behavior of small cracks emanating from notches is known. Several expressions have been proposed to model the dependency between the threshold value Δ
K
th of the stress intensity range and the crack size
a for very small cracks. Most of these expressions are based on length parameters, estimated from Δ
K
th and Δ
σ
0, resulting in a modified stress intensity range able to reproduce most of the behavior shown in the Kitagawa–Takahashi plot. Peterson or Topper-like expressions are then calibrated to
q based on these crack propagation estimates. However, such
q calibration is found to be extremely sensitive to the choice of Δ
K
th(
a) estimate. In this work, a generalization version of El Haddad–Topper–Smith’s equation is used to evaluate the behavior of cracks emanating from circular holes and semi-elliptical notches. For several combinations of notch dimensions, the smallest stress range necessary to both initiate and propagate a crack is calculated, resulting in expressions for
K
f and therefore for
q. It is found that the
q estimates obtained from this generalization, besides providing a sound physical basis for the notch sensitivity concept, better correlate with experimental data from the literature.</description><identifier>ISSN: 0142-1123</identifier><identifier>EISSN: 1879-3452</identifier><identifier>DOI: 10.1016/j.ijfatigue.2007.02.022</identifier><identifier>CODEN: IJFADB</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Applied sciences ; Exact sciences and technology ; Fatigue ; Fatigue crack growth threshold ; Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology ; Metals. Metallurgy ; Non-propagating cracks ; Notch sensitivity ; Short cracks</subject><ispartof>International journal of fatigue, 2007-09, Vol.29 (9), p.2022-2031</ispartof><rights>2007 Elsevier Ltd</rights><rights>2007 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c376t-8c3a253a455372c6c30b81c3d55ec928ee06346293fedd844643dfa94771366b3</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,310,314,780,784,789,790,23930,23931,25140,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=19069127$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Meggiolaro, Marco Antonio</creatorcontrib><creatorcontrib>Miranda, Antonio Carlos de Oliveira</creatorcontrib><creatorcontrib>de Castro, Jaime Tupiassú Pinho</creatorcontrib><title>Short crack threshold estimates to predict notch sensitivity factors in fatigue</title><title>International journal of fatigue</title><description>The notch sensitivity factor
q can be associated with the presence of non-propagating fatigue cracks at the notch root. Such cracks are present when the nominal stress range Δ
σ
n is between Δ
σ
0/
K
t and Δ
σ
0/
K
f, where Δ
σ
0 is the fatigue limit,
K
t is the geometric and
K
f is the fatigue stress concentration factors of the notch. Therefore, in principle it is possible to obtain expressions for
q if the propagation behavior of small cracks emanating from notches is known. Several expressions have been proposed to model the dependency between the threshold value Δ
K
th of the stress intensity range and the crack size
a for very small cracks. Most of these expressions are based on length parameters, estimated from Δ
K
th and Δ
σ
0, resulting in a modified stress intensity range able to reproduce most of the behavior shown in the Kitagawa–Takahashi plot. Peterson or Topper-like expressions are then calibrated to
q based on these crack propagation estimates. However, such
q calibration is found to be extremely sensitive to the choice of Δ
K
th(
a) estimate. In this work, a generalization version of El Haddad–Topper–Smith’s equation is used to evaluate the behavior of cracks emanating from circular holes and semi-elliptical notches. For several combinations of notch dimensions, the smallest stress range necessary to both initiate and propagate a crack is calculated, resulting in expressions for
K
f and therefore for
q. It is found that the
q estimates obtained from this generalization, besides providing a sound physical basis for the notch sensitivity concept, better correlate with experimental data from the literature.</description><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Fatigue</subject><subject>Fatigue crack growth threshold</subject><subject>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</subject><subject>Metals. Metallurgy</subject><subject>Non-propagating cracks</subject><subject>Notch sensitivity</subject><subject>Short cracks</subject><issn>0142-1123</issn><issn>1879-3452</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2007</creationdate><recordtype>article</recordtype><recordid>eNqFUMtKAzEUDaJgfXyD2ehual6TzCxL8QVCF-o6xDt3bOo4qUkq-PemtOhSOHA359zzIOSCsylnXF-vpn7Vu-zfNjgVjJkpEwXigEx4Y9pKqlockgnjSlScC3lMTlJaMcZaZuoJWTwtQ8wUooN3mpcR0zIMHcWU_YfLmGgOdB2x85DpGDIsacIx-ey_fP6mvYMcYqJ-pPsIZ-Sod0PC8_09JS-3N8_z--pxcfcwnz1WII3OVQPSiVo6VdfSCNAg2WvDQXZ1jdCKBpFpqbRoZY9d1yillex61ypjuNT6VZ6Sq93fdQyfmxLXfvgEOAxuxLBJVrLStZGqEM2OCDGkFLG361iqxW_Lmd0OaFf2d0C7HdAyUSCK8nJv4RK4oY9uBJ_-5C3TLRem8GY7Hpa-Xx6jTeBxhDJaRMi2C_5frx86pYs4</recordid><startdate>20070901</startdate><enddate>20070901</enddate><creator>Meggiolaro, Marco Antonio</creator><creator>Miranda, Antonio Carlos de Oliveira</creator><creator>de Castro, Jaime Tupiassú Pinho</creator><general>Elsevier Ltd</general><general>Elsevier Science</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>20070901</creationdate><title>Short crack threshold estimates to predict notch sensitivity factors in fatigue</title><author>Meggiolaro, Marco Antonio ; Miranda, Antonio Carlos de Oliveira ; de Castro, Jaime Tupiassú Pinho</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c376t-8c3a253a455372c6c30b81c3d55ec928ee06346293fedd844643dfa94771366b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2007</creationdate><topic>Applied sciences</topic><topic>Exact sciences and technology</topic><topic>Fatigue</topic><topic>Fatigue crack growth threshold</topic><topic>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</topic><topic>Metals. Metallurgy</topic><topic>Non-propagating cracks</topic><topic>Notch sensitivity</topic><topic>Short cracks</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Meggiolaro, Marco Antonio</creatorcontrib><creatorcontrib>Miranda, Antonio Carlos de Oliveira</creatorcontrib><creatorcontrib>de Castro, Jaime Tupiassú Pinho</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>International journal of fatigue</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Meggiolaro, Marco Antonio</au><au>Miranda, Antonio Carlos de Oliveira</au><au>de Castro, Jaime Tupiassú Pinho</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Short crack threshold estimates to predict notch sensitivity factors in fatigue</atitle><jtitle>International journal of fatigue</jtitle><date>2007-09-01</date><risdate>2007</risdate><volume>29</volume><issue>9</issue><spage>2022</spage><epage>2031</epage><pages>2022-2031</pages><issn>0142-1123</issn><eissn>1879-3452</eissn><coden>IJFADB</coden><abstract>The notch sensitivity factor
q can be associated with the presence of non-propagating fatigue cracks at the notch root. Such cracks are present when the nominal stress range Δ
σ
n is between Δ
σ
0/
K
t and Δ
σ
0/
K
f, where Δ
σ
0 is the fatigue limit,
K
t is the geometric and
K
f is the fatigue stress concentration factors of the notch. Therefore, in principle it is possible to obtain expressions for
q if the propagation behavior of small cracks emanating from notches is known. Several expressions have been proposed to model the dependency between the threshold value Δ
K
th of the stress intensity range and the crack size
a for very small cracks. Most of these expressions are based on length parameters, estimated from Δ
K
th and Δ
σ
0, resulting in a modified stress intensity range able to reproduce most of the behavior shown in the Kitagawa–Takahashi plot. Peterson or Topper-like expressions are then calibrated to
q based on these crack propagation estimates. However, such
q calibration is found to be extremely sensitive to the choice of Δ
K
th(
a) estimate. In this work, a generalization version of El Haddad–Topper–Smith’s equation is used to evaluate the behavior of cracks emanating from circular holes and semi-elliptical notches. For several combinations of notch dimensions, the smallest stress range necessary to both initiate and propagate a crack is calculated, resulting in expressions for
K
f and therefore for
q. It is found that the
q estimates obtained from this generalization, besides providing a sound physical basis for the notch sensitivity concept, better correlate with experimental data from the literature.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.ijfatigue.2007.02.022</doi><tpages>10</tpages></addata></record> |
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source | ScienceDirect Freedom Collection 2022-2024 |
subjects | Applied sciences Exact sciences and technology Fatigue Fatigue crack growth threshold Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology Metals. Metallurgy Non-propagating cracks Notch sensitivity Short cracks |
title | Short crack threshold estimates to predict notch sensitivity factors in fatigue |
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