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dc.contributor.authorBrian R. Daubenspeck
dc.contributor.authorAli P. Gordon
dc.date.accessioned2017-05-09T00:44:02Z
dc.date.available2017-05-09T00:44:02Z
dc.date.copyrightApril, 2011
dc.date.issued2011
dc.identifier.issn0094-4289
dc.identifier.otherJEMTA8-27139#021023_1.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/146192
dc.description.abstractA combination of extrapolation and estimation techniques from both prior and current studies has been explored with the goal of developing a method to accurately characterize high-stress amplitude low cycle fatigue of a material commonly used in gas turbine blades with the absence of such data. This paper describes innovative methods used to predict high-temperature fatigue of IN738LC, a dual-phase Ni-base superalloy. Three sets of experimental data at different temperatures are used to evaluate and examine the validity of extrapolation methods such as anchor points and hysteresis energy trends. High-stress amplitude data points approaching the ultimate strength of the material were added to pre-existing base data with limited plastic strain to achieve a full-range data set that could be used to test the legitimacy of the different prediction methods. Each method is evaluated at a number of temperatures.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleExtrapolation Techniques for Very Low Cycle Fatigue Behavior of a Ni-base Superalloy
dc.typeJournal Paper
dc.journal.volume133
dc.journal.issue2
dc.journal.titleJournal of Engineering Materials and Technology
dc.identifier.doi10.1115/1.4003602
dc.journal.fristpage21023
dc.identifier.eissn1528-8889
dc.keywordsFatigue
dc.keywordsTemperature
dc.keywordsSuperalloys
dc.keywordsStress
dc.keywordsLow cycle fatigue
dc.keywordsHigh temperature
dc.keywordsCycles AND Equations
dc.treeJournal of Engineering Materials and Technology:;2011:;volume( 133 ):;issue: 002
dc.contenttypeFulltext


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