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contributor authorBrian R. Daubenspeck
contributor authorAli P. Gordon
date accessioned2017-05-09T00:44:02Z
date available2017-05-09T00:44:02Z
date copyrightApril, 2011
date issued2011
identifier issn0094-4289
identifier otherJEMTA8-27139#021023_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/146192
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.
publisherThe American Society of Mechanical Engineers (ASME)
titleExtrapolation Techniques for Very Low Cycle Fatigue Behavior of a Ni-base Superalloy
typeJournal Paper
journal volume133
journal issue2
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.4003602
journal fristpage21023
identifier eissn1528-8889
keywordsFatigue
keywordsTemperature
keywordsSuperalloys
keywordsStress
keywordsLow cycle fatigue
keywordsHigh temperature
keywordsCycles AND Equations
treeJournal of Engineering Materials and Technology:;2011:;volume( 133 ):;issue: 002
contenttypeFulltext


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