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contributor authorJ. J. Pernot
contributor authorS. Mall
contributor authorT. Nicholas
date accessioned2017-05-08T23:47:24Z
date available2017-05-08T23:47:24Z
date copyrightJanuary, 1995
date issued1995
identifier issn0094-4289
identifier otherJEMTA8-26969#118_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/115437
description abstractObservations of isothermal fatigue, isothermal fatigue with superimposed load hold times, and thermomechanical fatigue (TMF) crack growth rate behavior of Ti-24Al-11Nb are presented and compared with results from previous studies on titanium and nickel-base superalloys. Elevated-temperature crack growth mechanisms in this alloy, which involve fatigue, oxidation and creep, and the influence of frequency, temperature, and hold-time are discussed. These mechanisms are used to interpret the observations of TMF crack growth. The limitations of current crack growth rate models based on the linear-elastic fracture mechanics parameter, K, are addressed.
publisherThe American Society of Mechanical Engineers (ASME)
titleCrack Growth Rate Behavior of a Titanium-Aluminide Alloy During Isothermal and Nonisothermal Conditions
typeJournal Paper
journal volume117
journal issue1
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2804362
journal fristpage118
journal lastpage126
identifier eissn1528-8889
keywordsAlloys
keywordsFracture (Materials)
keywordsTitanium aluminide
keywordsFatigue
keywordsTemperature
keywordsMechanisms
keywordsTitanium
keywordsNickel
keywordsCreep
keywordsFracture mechanics
keywordsoxidation
keywordsSuperalloys AND Stress
treeJournal of Engineering Materials and Technology:;1995:;volume( 117 ):;issue: 001
contenttypeFulltext


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