Multi-axial creep-fatigue life prediction considering history-dependent damage evolution : a new numerical procedure and experimental validation
Wang, Run-Zi and Guo, Su-Juan and Chen, Haofeng and Wen, Jian-Feng and Zhang, Xian-Cheng and Tu, Shan-Tung (2019) Multi-axial creep-fatigue life prediction considering history-dependent damage evolution : a new numerical procedure and experimental validation. Journal of the Mechanics and Physics of Solids, 131. pp. 313-336. ISSN 0022-5096 (https://doi.org/10.1016/j.jmps.2019.04.016)
Preview |
Text.
Filename: Wang_etal_JMPS_2019_Multi_axial_creep_fatigue_life_prediction_considering_history_dependent_damage_evolution.pdf
Accepted Author Manuscript License: Download (5MB)| Preview |
Abstract
In this paper, a new numerical procedure based on a cycle-by-cycle analysis has been constructed for creep-fatigue behavior and life prediction of high-temperature structures under multi-axial stress states. Within this framework, a modified unified viscoplastic constitutive model with isotropic hardening and modified kinematic hardening rules is developed to simulate the cycle-by-cycle stress-strain responses.Moreover, the newly constructed creep-fatigue approach calculates fatigue and creep damage variables using the critical plane method (CPM) and the modified strain energy density exhaustion (SEDE) model, respectively. The multi-axial ductility factor and elastic follow-up factor are also introduced into the modified SEDE model to accommodate the special multi-axial and mixed controlled modes, which are widely existed in practical structures. In order to validate the feasibility of the proposed numerical procedure, a series of creep-fatigue tests of notched specimens made from nickel-based GH4169 superalloy were carried out at 650 °C. The predicted numbers of cycles to crack initiation agree well with the experimental data. Evidence of crack initiation under various loading conditions was observed via the electron backscatter diffraction (EBSD) technique, indicating location-dependent crack initiations depending on loading conditions. In detail, the crack initiation sites shifting from surface to subsurface with increasing hold times can be well simulated by the proposed numerical procedure due to a reasonable description of the creep- fatigue damage evolution.
ORCID iDs
Wang, Run-Zi, Guo, Su-Juan, Chen, Haofeng ORCID: https://orcid.org/0000-0001-6864-4927, Wen, Jian-Feng, Zhang, Xian-Cheng and Tu, Shan-Tung;-
-
Item type: Article ID code: 67714 Dates: DateEvent31 October 2019Published30 April 2019Published Online29 April 2019AcceptedSubjects: Technology > Mechanical engineering and machinery Department: Faculty of Engineering > Mechanical and Aerospace Engineering Depositing user: Pure Administrator Date deposited: 07 May 2019 13:21 Last modified: 19 Nov 2024 16:54 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/67714