Assessing the Accuracy of Time‐Fraction and Ductility Exhaustion Approaches for Creep‐Fatigue Damage Prediction in Alloy 617 Through Feature Test Validation

ABSTRACT Determining creep‐fatigue damage formation is critical for elevated temperature components integrity. This study evaluates creep‐fatigue assessments with emphasis on differences between creep damage models. Evaluated are the time‐fraction model and the classical and stress‐modified ductility exhaustion creep damage models. This work extends the domain of stress‐modified ductility exhaustion models by introducing and validating such formalism to Ni‐based alloys. The fidelity of the assessments was benchmarked against uniaxial creep‐fatigue and multiaxial feature tests of Alloy 617. For uniaxial specimens, best estimate predictions rank ductility exhaustion as the most accurate and precise and time‐fraction as markedly conservative. For feature tests, ductility exhaustion predictions are within < 4.0 times difference, whereas time‐fraction underpredicts life by factors of 7–14. The observations suggest ductility exhaustion models as alternative to time‐fraction models in design codes for situations requiring characterization of the design margin. Further work in employing such models to assess other relevant phenomena (e.g., stress relaxation cracking) is discussed.

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Publication Details

Journal
Fatigue & Fracture of Engineering Materials & Structures
Published
2026-03-26
DOI
https://doi.org/10.1111/ffe.70266
Primary Topic
High Temperature Alloys and Creep
Type
article
Field-Weighted Citation Impact
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article

Assessing the Accuracy of Time‐Fraction and Ductility Exhaustion Approaches for Creep‐Fatigue Damage Prediction in Alloy 617 Through Feature Test Validation

Mark Messner, M. W. Spindler, M. Petkov
Fatigue & Fracture of Engineering Materials & Structures
High Temperature Alloys and Creep
article

Assessing the Accuracy of Time‐Fraction and Ductility Exhaustion Approaches for Creep‐Fatigue Damage Prediction in Alloy 617 Through Feature Test Validation

Mark Messner, M. W. Spindler, M. Petkov
article en

Abstract

ABSTRACT Determining creep‐fatigue damage formation is critical for elevated temperature components integrity. This study evaluates creep‐fatigue assessments with emphasis on differences between creep damage models. Evaluated are the time‐fraction model and the classical and stress‐modified ductility exhaustion creep damage models. This work extends the domain of stress‐modified ductility exhaustion models by introducing and validating such formalism to Ni‐based alloys. The fidelity of the assessments was benchmarked against uniaxial creep‐fatigue and multiaxial feature tests of Alloy 617. For uniaxial specimens, best estimate predictions rank ductility exhaustion as the most accurate and precise and time‐fraction as markedly conservative. For feature tests, ductility exhaustion predictions are within < 4.0 times difference, whereas time‐fraction underpredicts life by factors of 7–14. The observations suggest ductility exhaustion models as alternative to time‐fraction models in design codes for situations requiring characterization of the design margin. Further work in employing such models to assess other relevant phenomena (e.g., stress relaxation cracking) is discussed.

Fatigue & Fracture of Engineering Materials & Structures
Argonne National Laboratory (US), EDF Energy (United Kingdom) (GB), Rolls-Royce (United Kingdom) (GB)
Openalex Percentile: Top 8%
High Temperature Alloys and Creep
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