High Temperature Fatigue

Antolovich, Stephen D.; Pineau, A.

doi:10.1002/9781118616789.ch1

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Cyclic Softening1

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2016

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Cited by 4 publications

(1 citation statement)

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“…where A c is the cracked area, A o is the cross sectional area of the specimen, and LD is the load drop in a strain-controlled test [25]. Thus the majority of the cyclic softening, particularly that occurring early in life, cannot be accounted for by the grain boundary separation and surface cracking and instead more complex mechanisms are at play.…”

Section: Cyclic Softeningmentioning

confidence: 99%

The development of microstructural damage during high temperature creep–fatigue of a nickel alloy

Carroll

Cabet

Carroll

et al. 2013

International Journal of Fatigue

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Section: Cyclic Softeningmentioning

confidence: 99%

The development of microstructural damage during high temperature creep–fatigue of a nickel alloy

Carroll

Cabet

Carroll

et al. 2013

International Journal of Fatigue

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Creep–Fatigue Interactions (Crack Initiation)

Skelton

2016

Reference Module in Materials Science and Materials Engineering

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High temperature fatigue: behaviour of three typical classes of structural materials

Pineau

Antolovich

2015

Materials at High Temperatures

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The goals of this paper are: (i) to review the mechanisms of cyclic deformation, damage accumulation and crack propagation in three types of materials widely used in power generation industries, i.e. Cr-Mo steels, austenitic stainless steels and superalloys used in jet engine turbines (both Ni base and Fe-Ni base) when they are tested at elevated temperature; (ii) to relate these mechanisms to engineering applications; (iii) to review life prediction methodologies including thermomechanical fatigue (TMF); and (iv) to point out current and likely future trends in the development of more fatigue resistant materials and life prediction methods. The emphasis is laid on the creep-fatigue-oxidation behaviour of the two first classes of materials, i.e. 9-12% martensitic Cr steels and austenitic stainless steels. As the major issue for the design of components used in power generation industries is the extrapolation of short term laboratory data to much longer times, only physically based models for life prediction are examined. In Ni base superalloys, the emphasis is laid on the effect of oxidation on fatigue crack growth rate at elevated temperature and on their behaviour in TMF

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High Temperature Fatigue

Cited by 4 publications

References 68 publications

The development of microstructural damage during high temperature creep–fatigue of a nickel alloy

The development of microstructural damage during high temperature creep–fatigue of a nickel alloy

Creep–Fatigue Interactions (Crack Initiation)

High temperature fatigue: behaviour of three typical classes of structural materials

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