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    Development of an Improved High Cycle Fatigue Criterion

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001::page 162
    Author:
    Onome Scott-Emuakpor
    ,
    Tommy George
    ,
    Charles J. Cross
    ,
    M.-H. Herman Shen
    ,
    Jeffrey Calcaterra
    DOI: 10.1115/1.2360599
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An integrated computational-experimental approach for prediction of total fatigue life applied to a uniaxial stress state is developed. The approach consists of the following elements: (1) development of a vibration based fatigue testing procedure to achieve low cost bending fatigue experiments and (2) development of a life prediction and estimation implementation scheme for calculating effective fatigue cycles. A series of fully reversed bending fatigue tests were carried out using a vibration-based testing procedure to investigate the effects of bending stress on fatigue limit. The results indicate that the fatigue limit for 6061-T6 aluminum is approximately 20% higher than the respective limit in fully reversed tension-compression (axial). To validate the experimental observations and further evaluate the possibility of prediction of fatigue life, an improved high cycle fatigue criterion has been developed, which allows one to systematically determine the fatigue life based on the amount of energy loss per fatigue cycle. A comparison between the prediction and the experimental results was conducted and shows that the criterion is capable of providing accurate fatigue life prediction.
    keyword(s): Fatigue , Stress , Compression , Cycles , Tension , Fatigue testing , Fatigue life , Aluminum , Fatigue limit AND Vibration ,
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      Development of an Improved High Cycle Fatigue Criterion

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    http://yetl.yabesh.ir/yetl1/handle/yetl/135783
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    contributor authorOnome Scott-Emuakpor
    contributor authorTommy George
    contributor authorCharles J. Cross
    contributor authorM.-H. Herman Shen
    contributor authorJeffrey Calcaterra
    date accessioned2017-05-09T00:23:49Z
    date available2017-05-09T00:23:49Z
    date copyrightJanuary, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26935#162_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135783
    description abstractAn integrated computational-experimental approach for prediction of total fatigue life applied to a uniaxial stress state is developed. The approach consists of the following elements: (1) development of a vibration based fatigue testing procedure to achieve low cost bending fatigue experiments and (2) development of a life prediction and estimation implementation scheme for calculating effective fatigue cycles. A series of fully reversed bending fatigue tests were carried out using a vibration-based testing procedure to investigate the effects of bending stress on fatigue limit. The results indicate that the fatigue limit for 6061-T6 aluminum is approximately 20% higher than the respective limit in fully reversed tension-compression (axial). To validate the experimental observations and further evaluate the possibility of prediction of fatigue life, an improved high cycle fatigue criterion has been developed, which allows one to systematically determine the fatigue life based on the amount of energy loss per fatigue cycle. A comparison between the prediction and the experimental results was conducted and shows that the criterion is capable of providing accurate fatigue life prediction.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment of an Improved High Cycle Fatigue Criterion
    typeJournal Paper
    journal volume129
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2360599
    journal fristpage162
    journal lastpage169
    identifier eissn0742-4795
    keywordsFatigue
    keywordsStress
    keywordsCompression
    keywordsCycles
    keywordsTension
    keywordsFatigue testing
    keywordsFatigue life
    keywordsAluminum
    keywordsFatigue limit AND Vibration
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001
    contenttypeFulltext
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