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Novel method for the fatigue strength assessment of heavy sections made by ductile cast iron in presence of solidification defects
- Source :
- Fatigue & Fracture of Engineering Materials & Structures
- Publication Year :
- 2018
-
Abstract
- The fatigue strength of ferritic, pearlitic, and solution strengthened ferritic ductile irons taken from heavy sections and characterized by long solidification times has been assessed. Starting from the idea of Murakami and co‐workers, a new model for the prediction of the fatigue strength is proposed. It allows a sound fatigue assessment of the fatigue strength of as‐cast ductile irons containing solidification defects, such as low nodule count, exploded, chunky and spiky graphite, or microshrinkage porosities. The newly developed equation validated by means of an extensive benchmarking with data taken from the literature has shown a very high potential for applications to thick‐walled components. This is the pre-peer reviewed version of an article, which has been published in final form at [https://doi.org/10.1111/ffe.12815]. This article may be used for non-commercial purposes in accordance with Wiley Terms and Conditions for Self-Archiving.
- Subjects :
- fatigue strength assessment
Materials science
solidification defects
nodular iron
02 engineering and technology
engineering.material
mechanical properties
ductility
extensive benchmarking
benchmarking
defects
fatigue of materials
ferrite
solidification, defect assessment
ductile cast irons
fatigue assessments
fatigue life prediction
fatigue strength
solidification defects, cast iron
defect assessment
fatigue
0203 mechanical engineering
General Materials Science
Mechanical Engineering
Metallurgy
021001 nanoscience & nanotechnology
Fatigue limit
cast iron
020303 mechanical engineering & transports
Mechanics of Materials
engineering
Cast iron
solidification
0210 nano-technology
Subjects
Details
- Language :
- English
- Database :
- OpenAIRE
- Journal :
- Fatigue & Fracture of Engineering Materials & Structures
- Accession number :
- edsair.doi.dedup.....dd5425c6f303e7dabbf69c93cc76c70c