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contributor authorJ. N. Yang
contributor authorR. C. Donath
date accessioned2017-05-08T23:18:09Z
date available2017-05-08T23:18:09Z
date copyrightJanuary, 1984
date issued1984
identifier issn0094-4289
identifier otherJEMTA8-26896#79_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98577
description abstractA statistically-formulated fracture mechanics model for crack growth under sustained load is used to analyze crack growth data from 23 compact tension specimens of IN100, a turbojet engine disk material. The procedures characterize crack growth rates assuming that the growth rate is a lognormal random variable. The mean and standard deviation of the growth rate are determined from test data using the method of maximum likelihood. From these estimates, a lognormal creep crack growth rate model is developed from which is derived a statistical distribution of the crack size at any time. The distribution of time to reach some critical crack size is also presented. These distributions allow for the determination of the effect of hold time in the loading cycle on the life prediction of gas turbine engine disks.
publisherThe American Society of Mechanical Engineers (ASME)
titleStatistics of Crack Growth of a Superalloy Under Sustained Load
typeJournal Paper
journal volume106
journal issue1
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.3225680
journal fristpage79
journal lastpage83
identifier eissn1528-8889
keywordsSuperalloys
keywordsStress
keywordsFracture (Materials)
keywordsDisks
keywordsCycles
keywordsStatistical distributions
keywordsTension
keywordsTurbojets
keywordsGas turbines
keywordsCreep
keywordsFracture mechanics AND Engines
treeJournal of Engineering Materials and Technology:;1984:;volume( 106 ):;issue: 001
contenttypeFulltext


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