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contributor authorStorgأ¤rds, Erik
contributor authorSimonsson, Kjell
contributor authorSjأ¶strأ¶m, Sأ¶ren
contributor authorMoverare, Johan
date accessioned2017-05-09T01:27:58Z
date available2017-05-09T01:27:58Z
date issued2016
identifier issn1528-8919
identifier othergtp_138_01_012503.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/160966
description abstractThermomechanical fatigue (TMF) crack growth modeling has been conducted on Inconel 718 with dwell time at maximum load. A history dependent damage model taking dwell damage into account, developed under isothermal conditions, has been extended for TMF conditions. Parameter determination for the model is carried out on isothermal load controlled tests at 550–650 آ°C for surface cracks, which later have been used to extrapolate parameters used for TMF crack growth. Further, validation of the developed model is conducted on a notched specimen subjected to strain control at 50–550 آ°C. Satisfying results are gained within reasonable scatter level compared for test and simulated number of cycles to failure.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermomechanical Fatigue Crack Growth Modeling in a Ni Based Superalloy Subjected to Sustained Load
typeJournal Paper
journal volume138
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4031158
journal fristpage12503
journal lastpage12503
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 001
contenttypeFulltext


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