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    Mechanistic Model to Predict Statistical Scatter in Fatigue Response of Titanium Aluminide

    Source: Journal of Aerospace Engineering:;2001:;Volume ( 014 ):;issue: 004
    Author:
    Robert G. Tryon
    ,
    Animesh Dey
    DOI: 10.1061/(ASCE)0893-1321(2001)14:4(120)
    Publisher: American Society of Civil Engineers
    Abstract: This paper discusses research to develop a computer modeling technique to predict the statistical behavior of fatigue in fully lamellar TiAl. Probabilistic micromechanics was used to relate the random nature of the microstructure to the fatigue response of smooth round bar specimens. The effort showed that models proposed in the literature addressing the microstructural mechanisms that govern fatigue damage accumulation could be combined with the concept of mesomechanics to properly account for the characteristic sizes and multiple phases of fatigue. The capability developed can be used to virtually test large numbers of specimens for which actual laboratory testing would be cost prohibitive.
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      Mechanistic Model to Predict Statistical Scatter in Fatigue Response of Titanium Aluminide

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    contributor authorRobert G. Tryon
    contributor authorAnimesh Dey
    date accessioned2017-05-08T22:17:03Z
    date available2017-05-08T22:17:03Z
    date copyrightOctober 2001
    date issued2001
    identifier other40086040.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/76189
    description abstractThis paper discusses research to develop a computer modeling technique to predict the statistical behavior of fatigue in fully lamellar TiAl. Probabilistic micromechanics was used to relate the random nature of the microstructure to the fatigue response of smooth round bar specimens. The effort showed that models proposed in the literature addressing the microstructural mechanisms that govern fatigue damage accumulation could be combined with the concept of mesomechanics to properly account for the characteristic sizes and multiple phases of fatigue. The capability developed can be used to virtually test large numbers of specimens for which actual laboratory testing would be cost prohibitive.
    publisherAmerican Society of Civil Engineers
    titleMechanistic Model to Predict Statistical Scatter in Fatigue Response of Titanium Aluminide
    typeJournal Paper
    journal volume14
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2001)14:4(120)
    treeJournal of Aerospace Engineering:;2001:;Volume ( 014 ):;issue: 004
    contenttypeFulltext
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