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    Fatigue Performance of High-Pressure Waterjet-Peened Aluminum Alloy

    Source: Journal of Pressure Vessel Technology:;2002:;volume( 124 ):;issue: 001::page 118
    Author:
    M. Ramulu
    ,
    M. Hashish
    ,
    J. Hopkins
    ,
    S. Kunaporn
    ,
    M. Jenkins
    DOI: 10.1115/1.1398553
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study of high-pressure waterjet peening on 7075-T6 aluminum alloy was conducted to investigate the effects of waterjet on high-cycle fatigue life and fatigue crack growth. Unnotched hourglass-shaped circular cross section test specimens were fatigue tested in completely reversed rotating bending (R=Smin/Smax=−1) to determine fatigue life behavior (S-N curves). Single-edge-notched flat tensile test specimens were tested in the tension-tension fatigue crack growth tests (R=Smin/Smax=0.1) to determine fatigue crack propagation behavior (da/dN versus ΔK). Surface characteristics and fracture surfaces were evaluated by scanning electron microscopy (SEM). Results show that waterjet peening can increase high-cycle fatigue life, delay fatigue crack initiation, and decrease the rate of fatigue crack propagation.
    keyword(s): Fatigue , Aluminum alloys , Shot peening , High pressure (Physics) , Cycles , Fatigue cracks , Fatigue life , Fracture (Process) , Stress , Tension , Deformation AND Delays ,
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      Fatigue Performance of High-Pressure Waterjet-Peened Aluminum Alloy

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/127386
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    • Journal of Pressure Vessel Technology

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    contributor authorM. Ramulu
    contributor authorM. Hashish
    contributor authorJ. Hopkins
    contributor authorS. Kunaporn
    contributor authorM. Jenkins
    date accessioned2017-05-09T00:08:33Z
    date available2017-05-09T00:08:33Z
    date copyrightFebruary, 2002
    date issued2002
    identifier issn0094-9930
    identifier otherJPVTAS-28414#118_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/127386
    description abstractAn experimental study of high-pressure waterjet peening on 7075-T6 aluminum alloy was conducted to investigate the effects of waterjet on high-cycle fatigue life and fatigue crack growth. Unnotched hourglass-shaped circular cross section test specimens were fatigue tested in completely reversed rotating bending (R=Smin/Smax=−1) to determine fatigue life behavior (S-N curves). Single-edge-notched flat tensile test specimens were tested in the tension-tension fatigue crack growth tests (R=Smin/Smax=0.1) to determine fatigue crack propagation behavior (da/dN versus ΔK). Surface characteristics and fracture surfaces were evaluated by scanning electron microscopy (SEM). Results show that waterjet peening can increase high-cycle fatigue life, delay fatigue crack initiation, and decrease the rate of fatigue crack propagation.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFatigue Performance of High-Pressure Waterjet-Peened Aluminum Alloy
    typeJournal Paper
    journal volume124
    journal issue1
    journal titleJournal of Pressure Vessel Technology
    identifier doi10.1115/1.1398553
    journal fristpage118
    journal lastpage123
    identifier eissn1528-8978
    keywordsFatigue
    keywordsAluminum alloys
    keywordsShot peening
    keywordsHigh pressure (Physics)
    keywordsCycles
    keywordsFatigue cracks
    keywordsFatigue life
    keywordsFracture (Process)
    keywordsStress
    keywordsTension
    keywordsDeformation AND Delays
    treeJournal of Pressure Vessel Technology:;2002:;volume( 124 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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