THE ETM METHOD FOR ASSESSING THE SIGNIFICANCE OF CRACK-LIKE DEFECTS IN ENGINEERING STRUCTURES
The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the cra...
Ausführliche Beschreibung
Autor*in: |
Schwalbe [verfasserIn] Zerbst [verfasserIn] Brocks [verfasserIn] |
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Format: |
E-Artikel |
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Erschienen: |
Oxford, UK: Blackwell Science Ltd ; 1998 |
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Schlagwörter: |
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Umfang: |
Online-Ressource |
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Reproduktion: |
2008 ; Blackwell Publishing Journal Backfiles 1879-2005 |
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Übergeordnetes Werk: |
In: Fatigue & fracture of engineering materials & structures - Oxford [u.a.] : Wiley-Blackwell, 1979, 21(1998), 10, Seite 0 |
Übergeordnetes Werk: |
volume:21 ; year:1998 ; number:10 ; pages:0 |
Links: |
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DOI / URN: |
10.1046/j.1460-2695.1998.00112.x |
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10.1046/j.1460-2695.1998.00112.x doi (DE-627)NLEJ242943020 DE-627 ger DE-627 rakwb Schwalbe verfasserin aut THE ETM METHOD FOR ASSESSING THE SIGNIFICANCE OF CRACK-LIKE DEFECTS IN ENGINEERING STRUCTURES Oxford, UK Blackwell Science Ltd 1998 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain. 2008 Blackwell Publishing Journal Backfiles 1879-2005 |2008|||||||||| Crack driving force Zerbst verfasserin aut Brocks verfasserin aut Cornec oth Heerens oth Amstutz oth In Fatigue & fracture of engineering materials & structures Oxford [u.a.] : Wiley-Blackwell, 1979 21(1998), 10, Seite 0 Online-Ressource (DE-627)NLEJ243926898 (DE-600)2014746-6 1460-2695 nnns volume:21 year:1998 number:10 pages:0 http://dx.doi.org/10.1046/j.1460-2695.1998.00112.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 21 1998 10 0 |
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10.1046/j.1460-2695.1998.00112.x doi (DE-627)NLEJ242943020 DE-627 ger DE-627 rakwb Schwalbe verfasserin aut THE ETM METHOD FOR ASSESSING THE SIGNIFICANCE OF CRACK-LIKE DEFECTS IN ENGINEERING STRUCTURES Oxford, UK Blackwell Science Ltd 1998 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain. 2008 Blackwell Publishing Journal Backfiles 1879-2005 |2008|||||||||| Crack driving force Zerbst verfasserin aut Brocks verfasserin aut Cornec oth Heerens oth Amstutz oth In Fatigue & fracture of engineering materials & structures Oxford [u.a.] : Wiley-Blackwell, 1979 21(1998), 10, Seite 0 Online-Ressource (DE-627)NLEJ243926898 (DE-600)2014746-6 1460-2695 nnns volume:21 year:1998 number:10 pages:0 http://dx.doi.org/10.1046/j.1460-2695.1998.00112.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 21 1998 10 0 |
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10.1046/j.1460-2695.1998.00112.x doi (DE-627)NLEJ242943020 DE-627 ger DE-627 rakwb Schwalbe verfasserin aut THE ETM METHOD FOR ASSESSING THE SIGNIFICANCE OF CRACK-LIKE DEFECTS IN ENGINEERING STRUCTURES Oxford, UK Blackwell Science Ltd 1998 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain. 2008 Blackwell Publishing Journal Backfiles 1879-2005 |2008|||||||||| Crack driving force Zerbst verfasserin aut Brocks verfasserin aut Cornec oth Heerens oth Amstutz oth In Fatigue & fracture of engineering materials & structures Oxford [u.a.] : Wiley-Blackwell, 1979 21(1998), 10, Seite 0 Online-Ressource (DE-627)NLEJ243926898 (DE-600)2014746-6 1460-2695 nnns volume:21 year:1998 number:10 pages:0 http://dx.doi.org/10.1046/j.1460-2695.1998.00112.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 21 1998 10 0 |
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10.1046/j.1460-2695.1998.00112.x doi (DE-627)NLEJ242943020 DE-627 ger DE-627 rakwb Schwalbe verfasserin aut THE ETM METHOD FOR ASSESSING THE SIGNIFICANCE OF CRACK-LIKE DEFECTS IN ENGINEERING STRUCTURES Oxford, UK Blackwell Science Ltd 1998 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain. 2008 Blackwell Publishing Journal Backfiles 1879-2005 |2008|||||||||| Crack driving force Zerbst verfasserin aut Brocks verfasserin aut Cornec oth Heerens oth Amstutz oth In Fatigue & fracture of engineering materials & structures Oxford [u.a.] : Wiley-Blackwell, 1979 21(1998), 10, Seite 0 Online-Ressource (DE-627)NLEJ243926898 (DE-600)2014746-6 1460-2695 nnns volume:21 year:1998 number:10 pages:0 http://dx.doi.org/10.1046/j.1460-2695.1998.00112.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 21 1998 10 0 |
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10.1046/j.1460-2695.1998.00112.x doi (DE-627)NLEJ242943020 DE-627 ger DE-627 rakwb Schwalbe verfasserin aut THE ETM METHOD FOR ASSESSING THE SIGNIFICANCE OF CRACK-LIKE DEFECTS IN ENGINEERING STRUCTURES Oxford, UK Blackwell Science Ltd 1998 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain. 2008 Blackwell Publishing Journal Backfiles 1879-2005 |2008|||||||||| Crack driving force Zerbst verfasserin aut Brocks verfasserin aut Cornec oth Heerens oth Amstutz oth In Fatigue & fracture of engineering materials & structures Oxford [u.a.] : Wiley-Blackwell, 1979 21(1998), 10, Seite 0 Online-Ressource (DE-627)NLEJ243926898 (DE-600)2014746-6 1460-2695 nnns volume:21 year:1998 number:10 pages:0 http://dx.doi.org/10.1046/j.1460-2695.1998.00112.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 21 1998 10 0 |
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THE ETM METHOD FOR ASSESSING THE SIGNIFICANCE OF CRACK-LIKE DEFECTS IN ENGINEERING STRUCTURES |
abstract |
The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain. |
abstractGer |
The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain. |
abstract_unstemmed |
The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain. |
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<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">NLEJ242943020</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20210707170320.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">120427s1998 xx |||||o 00| ||und c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1046/j.1460-2695.1998.00112.x</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)NLEJ242943020</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Schwalbe</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">THE ETM METHOD FOR ASSESSING THE SIGNIFICANCE OF CRACK-LIKE DEFECTS IN ENGINEERING STRUCTURES</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Oxford, UK</subfield><subfield code="b">Blackwell Science Ltd</subfield><subfield code="c">1998</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">nicht spezifiziert</subfield><subfield code="b">zzz</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">nicht spezifiziert</subfield><subfield code="b">z</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">nicht spezifiziert</subfield><subfield code="b">zu</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">The Engineering Flaw Assessment Method, EFAM, is presently being developed at GKSS. It consists of several individual documents for determining material properties and the crack driving force. The present paper briefly describes the document EFAM ETM 97 which provides guidance for estimating the crack tip opening displacement (CTOD) and the J-integral as driving force parameters for homogeneous structures. The CTOD and J can be expressed as functions of applied force or applied strain.</subfield></datafield><datafield tag="533" ind1=" " ind2=" "><subfield code="d">2008</subfield><subfield code="f">Blackwell Publishing Journal Backfiles 1879-2005</subfield><subfield code="7">|2008||||||||||</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Crack driving force</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Zerbst</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Brocks</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Cornec</subfield><subfield code="4">oth</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Heerens</subfield><subfield code="4">oth</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Amstutz</subfield><subfield code="4">oth</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">In</subfield><subfield code="t">Fatigue & fracture of engineering materials & structures</subfield><subfield code="d">Oxford [u.a.] : Wiley-Blackwell, 1979</subfield><subfield code="g">21(1998), 10, Seite 0</subfield><subfield code="h">Online-Ressource</subfield><subfield code="w">(DE-627)NLEJ243926898</subfield><subfield code="w">(DE-600)2014746-6</subfield><subfield code="x">1460-2695</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:21</subfield><subfield code="g">year:1998</subfield><subfield code="g">number:10</subfield><subfield code="g">pages:0</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">http://dx.doi.org/10.1046/j.1460-2695.1998.00112.x</subfield><subfield code="q">text/html</subfield><subfield code="x">Verlag</subfield><subfield code="z">Deutschlandweit zugänglich</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_U</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">ZDB-1-DJB</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_NL_ARTICLE</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">21</subfield><subfield code="j">1998</subfield><subfield code="e">10</subfield><subfield code="h">0</subfield></datafield></record></collection>
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