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    A Fatigue Crack Growth Model for Single Overload Tests

    Source: Journal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 002::page 168
    Author:
    H. S. Goel
    ,
    Satish Chand
    DOI: 10.1115/1.2904268
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Crack growth rate experiments are conducted by applying an intermediate single overload cycle in constant amplitude load (CAL) tests. For a particular overload ratio, three to four tests are conducted by applying the overload cycle at different crack lengths. The loads are selected in such a way that for a given overload ratio, the size of the overload and CAL monotonic plastic zones are the same at each crack length. A functional form for the crack growth during the retardation was developed that accurately describes all the tests. For comparison, the corresponding CA-load tests are also conducted separately. Finally, a crack growth rate model is developed.
    keyword(s): Stress , Fracture (Materials) , Cycles AND Fatigue cracks ,
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      A Fatigue Crack Growth Model for Single Overload Tests

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    http://yetl.yabesh.ir/yetl1/handle/yetl/113702
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    • Journal of Engineering Materials and Technology

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    contributor authorH. S. Goel
    contributor authorSatish Chand
    date accessioned2017-05-08T23:44:26Z
    date available2017-05-08T23:44:26Z
    date copyrightApril, 1994
    date issued1994
    identifier issn0094-4289
    identifier otherJEMTA8-26963#168_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113702
    description abstractCrack growth rate experiments are conducted by applying an intermediate single overload cycle in constant amplitude load (CAL) tests. For a particular overload ratio, three to four tests are conducted by applying the overload cycle at different crack lengths. The loads are selected in such a way that for a given overload ratio, the size of the overload and CAL monotonic plastic zones are the same at each crack length. A functional form for the crack growth during the retardation was developed that accurately describes all the tests. For comparison, the corresponding CA-load tests are also conducted separately. Finally, a crack growth rate model is developed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Fatigue Crack Growth Model for Single Overload Tests
    typeJournal Paper
    journal volume116
    journal issue2
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.2904268
    journal fristpage168
    journal lastpage172
    identifier eissn1528-8889
    keywordsStress
    keywordsFracture (Materials)
    keywordsCycles AND Fatigue cracks
    treeJournal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 002
    contenttypeFulltext
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