Strain‐Controlled Low‐Cycle Fatigue Behavior of a Superalloy Considering Extensive Temperature Range and Stress Concentration

ABSTRACT This study aims to investigate the low cycle fatigue (LCF) behavior and fatigue life prediction method of an advanced solid solution–strengthened nickel‐based superalloy at various temperatures and stress concentrations. Cylindrical specimens as well as plates with three types of holes (including straight holes and inclined holes with different orientations) were designed and machined for fatigue tests. The test results revealed fatigue life decreases with the temperature increasing. Meanwhile, the fatigue lives of the plate specimens have decreased differently and are strongly dependent on the geometry and orientation of the holes. The key damage parameter related to the fatigue life was found on the strain gradient path. A criterion based on strain gradient is defined as the boundary of the damage process zone. The results show that the prediction was in good agreement with the experimental data, for the majority of the data are within a scatter band of ±2.

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Publication Details

Journal
Fatigue & Fracture of Engineering Materials & Structures
Published
2024-11-11
DOI
https://doi.org/10.1111/ffe.14503
Citations
2
Primary Topic
High Temperature Alloys and Creep
Type
article
Field-Weighted Citation Impact
0.43
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article

Strain‐Controlled Low‐Cycle Fatigue Behavior of a Superalloy Considering Extensive Temperature Range and Stress Concentration

Xu Wang, Dong Mi, Qinzheng Yang, Wenjun Wang et al.
2 citations
Fatigue & Fracture of Engineering Materials & Structures
High Temperature Alloys and Creep
0.43
article

Strain‐Controlled Low‐Cycle Fatigue Behavior of a Superalloy Considering Extensive Temperature Range and Stress Concentration

Xu Wang, Dong Mi, Qinzheng Yang, Wenjun Wang, Lingying Luo
article en
2 citations

Abstract

ABSTRACT This study aims to investigate the low cycle fatigue (LCF) behavior and fatigue life prediction method of an advanced solid solution–strengthened nickel‐based superalloy at various temperatures and stress concentrations. Cylindrical specimens as well as plates with three types of holes (including straight holes and inclined holes with different orientations) were designed and machined for fatigue tests. The test results revealed fatigue life decreases with the temperature increasing. Meanwhile, the fatigue lives of the plate specimens have decreased differently and are strongly dependent on the geometry and orientation of the holes. The key damage parameter related to the fatigue life was found on the strain gradient path. A criterion based on strain gradient is defined as the boundary of the damage process zone. The results show that the prediction was in good agreement with the experimental data, for the majority of the data are within a scatter band of ±2.

Fatigue & Fracture of Engineering Materials & StructuresVol. 48(2)
Aero Engine Corporation of China (China) (CN), Nanchang Hangkong University (CN)
Responsible consumption and production
Openalex Percentile: Top 41%
High Temperature Alloys and Creep
0.43
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Strain‐Controlled Low‐Cycle Fatigue Behavior of a Superalloy Considering Extensive Temperature Range and Stress Concentration — Xu Wang, Dong Mi, et al. · Fatigue & Fracture of Engineering Materials & Structures (2024) | TGRS Research Map | TGRS