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    Frequency Effects in the Elevated Temperature Crack Growth Behavior of Austenitic Stainless Steels—A Design Approach

    Source: Journal of Pressure Vessel Technology:;1979:;volume( 101 ):;issue: 002::page 171
    Author:
    L. A. James
    DOI: 10.1115/1.3454617
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The fatigue-crack growth behavior of annealed types 304 and 316 stainless steels is determined over a range of cyclic frequencies in an air environment at temperatures of 800°F (427°C), 1000°F (538°C) and 1200°F (649°C). A good portion of the experimental data supports the observation that the fatigue crack growth rates at a given value of ΔK increases with decreasing frequencies. The behavior ot each temperature is normalized relative to the behavior at a “standard” frequency of 40 cpm, and a simple frequency correction factor is derived. This frequency correction factor, more applicable to type 304 than to 316 stainless steels, is further coupled with temperature effects data taken at the “standard” frequency and combined with a stress ratio correction to furnish estimates of the fatigue crack growth behavior of those two steels over a fairly wide range of parameters.
    keyword(s): Temperature , Fracture (Materials) , Design , Stainless steel , Fatigue cracks , Frequency , Steel , Stress AND Temperature effects ,
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      Frequency Effects in the Elevated Temperature Crack Growth Behavior of Austenitic Stainless Steels—A Design Approach

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    http://yetl.yabesh.ir/yetl1/handle/yetl/92589
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    contributor authorL. A. James
    date accessioned2017-05-08T23:07:32Z
    date available2017-05-08T23:07:32Z
    date copyrightMay, 1979
    date issued1979
    identifier issn0094-9930
    identifier otherJPVTAS-28173#171_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92589
    description abstractThe fatigue-crack growth behavior of annealed types 304 and 316 stainless steels is determined over a range of cyclic frequencies in an air environment at temperatures of 800°F (427°C), 1000°F (538°C) and 1200°F (649°C). A good portion of the experimental data supports the observation that the fatigue crack growth rates at a given value of ΔK increases with decreasing frequencies. The behavior ot each temperature is normalized relative to the behavior at a “standard” frequency of 40 cpm, and a simple frequency correction factor is derived. This frequency correction factor, more applicable to type 304 than to 316 stainless steels, is further coupled with temperature effects data taken at the “standard” frequency and combined with a stress ratio correction to furnish estimates of the fatigue crack growth behavior of those two steels over a fairly wide range of parameters.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFrequency Effects in the Elevated Temperature Crack Growth Behavior of Austenitic Stainless Steels—A Design Approach
    typeJournal Paper
    journal volume101
    journal issue2
    journal titleJournal of Pressure Vessel Technology
    identifier doi10.1115/1.3454617
    journal fristpage171
    journal lastpage176
    identifier eissn1528-8978
    keywordsTemperature
    keywordsFracture (Materials)
    keywordsDesign
    keywordsStainless steel
    keywordsFatigue cracks
    keywordsFrequency
    keywordsSteel
    keywordsStress AND Temperature effects
    treeJournal of Pressure Vessel Technology:;1979:;volume( 101 ):;issue: 002
    contenttypeFulltext
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