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    Statistics of Crack Growth of a Superalloy Under Sustained Load

    Source: Journal of Engineering Materials and Technology:;1984:;volume( 106 ):;issue: 001::page 79
    Author:
    J. N. Yang
    ,
    R. C. Donath
    DOI: 10.1115/1.3225680
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A statistically-formulated fracture mechanics model for crack growth under sustained load is used to analyze crack growth data from 23 compact tension specimens of IN100, a turbojet engine disk material. The procedures characterize crack growth rates assuming that the growth rate is a lognormal random variable. The mean and standard deviation of the growth rate are determined from test data using the method of maximum likelihood. From these estimates, a lognormal creep crack growth rate model is developed from which is derived a statistical distribution of the crack size at any time. The distribution of time to reach some critical crack size is also presented. These distributions allow for the determination of the effect of hold time in the loading cycle on the life prediction of gas turbine engine disks.
    keyword(s): Superalloys , Stress , Fracture (Materials) , Disks , Cycles , Statistical distributions , Tension , Turbojets , Gas turbines , Creep , Fracture mechanics AND Engines ,
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      Statistics of Crack Growth of a Superalloy Under Sustained Load

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    http://yetl.yabesh.ir/yetl1/handle/yetl/98577
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    contributor authorJ. N. Yang
    contributor authorR. C. Donath
    date accessioned2017-05-08T23:18:09Z
    date available2017-05-08T23:18:09Z
    date copyrightJanuary, 1984
    date issued1984
    identifier issn0094-4289
    identifier otherJEMTA8-26896#79_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98577
    description abstractA statistically-formulated fracture mechanics model for crack growth under sustained load is used to analyze crack growth data from 23 compact tension specimens of IN100, a turbojet engine disk material. The procedures characterize crack growth rates assuming that the growth rate is a lognormal random variable. The mean and standard deviation of the growth rate are determined from test data using the method of maximum likelihood. From these estimates, a lognormal creep crack growth rate model is developed from which is derived a statistical distribution of the crack size at any time. The distribution of time to reach some critical crack size is also presented. These distributions allow for the determination of the effect of hold time in the loading cycle on the life prediction of gas turbine engine disks.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStatistics of Crack Growth of a Superalloy Under Sustained Load
    typeJournal Paper
    journal volume106
    journal issue1
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.3225680
    journal fristpage79
    journal lastpage83
    identifier eissn1528-8889
    keywordsSuperalloys
    keywordsStress
    keywordsFracture (Materials)
    keywordsDisks
    keywordsCycles
    keywordsStatistical distributions
    keywordsTension
    keywordsTurbojets
    keywordsGas turbines
    keywordsCreep
    keywordsFracture mechanics AND Engines
    treeJournal of Engineering Materials and Technology:;1984:;volume( 106 ):;issue: 001
    contenttypeFulltext
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