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Effects of temperature and strain rate on isothermal low-cycle fatigue behaviour of Inconel 718 superalloy: Damage mechanisms, microstructure evolution, and life prediction

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68081723%3A_____%2F25%3A00619415" target="_blank" >RIV/68081723:_____/25:00619415 - isvavai.cz</a>

  • Alternative codes found

    RIV/68407700:21220/25:00384522

  • Result on the web

    <a href="https://www.webofscience.com/wos/woscc/full-record/WOS:001488516100001" target="_blank" >https://www.webofscience.com/wos/woscc/full-record/WOS:001488516100001</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1016/j.ijfatigue.2025.109005" target="_blank" >10.1016/j.ijfatigue.2025.109005</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Effects of temperature and strain rate on isothermal low-cycle fatigue behaviour of Inconel 718 superalloy: Damage mechanisms, microstructure evolution, and life prediction

  • Original language description

    In this article, strain-controlled Low-Cycle Fatigue (LCF) tests were performed on Inconel 718 nickel-based superalloy at temperatures of 300 ◦C, 650 ◦C, and 730 ◦C. The LCF tests were conducted at various mechanical strain amplitudes between 3.5×10−3 and 1×10−2, and three different mechanical strain rates: 1×10−4/s, 1×10−3/s, and 1×10−2/s. Cyclic straining resulted in cyclic softening under all investigated loading conditions, with the effect being more significant at higher temperatures. The cyclic softening was attributed to the formation of persistent slip bands and the shearing of coherent precipitates. At 730 ◦C, delta phase precipitation in LCF tests conducted at low strain rates contributed to additional softening. Investigations into the damage mechanisms revealed that the predominant failure mode shifted from transgranular at 300 ◦C to intergranular at 650 ◦C and 730 ◦C. In addition, fatigue crack initiation sites most frequently involved broken or oxidized carbides. The fatigue lifetime decreased with an increasing temperature and a decreasing strain rate, primarily due to oxidation-assisted intergranular cracking at high temperatures, involving the formation of brittle oxides at grain boundaries. Finally, a multi-mechanism-based damage model was proposed to predict fatigue lifetime, accounting for contributions from oxidation, creep, and fatigue damage. The model exhibited a good correlation between the predicted and the observed lifetimes.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • OECD FORD branch

    20501 - Materials engineering

Result continuities

  • Project

    Result was created during the realization of more than one project. More information in the Projects tab.

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2025

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Name of the periodical

    International Journal of Fatigue

  • ISSN

    0142-1123

  • e-ISSN

    1879-3452

  • Volume of the periodical

    198

  • Issue of the periodical within the volume

    Sept

  • Country of publishing house

    GB - UNITED KINGDOM

  • Number of pages

    19

  • Pages from-to

    109005

  • UT code for WoS article

    001488516100001

  • EID of the result in the Scopus database

    2-s2.0-105003995909