Assessing Fatigue Life Cycles of Material X10CrMoVNb9-1 through a Combination of Experimental and Finite Element Analysis

Author:

Rahim Mohammad Ridzwan Bin Abd12ORCID,Schmauder Siegfried1ORCID,Manurung Yupiter H. P.3,Binkele Peter1ORCID,Dusza Ján4,Csanádi Tamás45,Ahmad Meor Iqram Meor6ORCID,Mat Muhd Faiz3ORCID,Dogahe Kiarash Jamali17ORCID

Affiliation:

1. Institute for Material Testing, Materials Science and Strength of Materials (IMWF), University of Stuttgart, 70569 Stuttgart, Germany

2. Department of Occupational Safety and Health (DOSH) Sarawak, Kuching 93100, Malaysia

3. Smart Manufacturing Research Institute (SMRI) and School of Mechanical Engineering, Universiti Teknologi MARA (UiTM), Shah Alam 40450, Malaysia

4. Institute of Materials Research of SAS, Watsonova 47, 040 01 Košice, Slovakia

5. Donát Bánki Faculty of Mechanical and Safety Engineering, Óbuda University, Népszínhás utca 8, 1081 Budapest, Hungary

6. Department of Mechanical and Manufacturing Engineering, Faculty of Engineering and Built Environment, Universiti Kebangsaan Malaysia (UKM), Bandar Baru Bangi 43600, Malaysia

7. Graduate School of Advanced Manufacturing Engineering (GSaME), University of Stuttgart, Nobelstraße 12, 70569 Stuttgart, Germany

Abstract

This paper uses a two-scale material modeling approach to investigate fatigue crack initiation and propagation of the material X10CrMoVNb9-1 (P91) under cyclic loading at room temperature. The Voronoi tessellation method was implemented to generate an artificial microstructure model at the microstructure level, and then, the finite element (FE) method was applied to identify different stress distributions. The stress distributions for multiple artificial microstructures was analyzed by using the physically based Tanaka–Mura model to estimate the number of cycles for crack initiation. Considering the prediction of macro-scale and long-term crack formation, the Paris law was utilized in this research. Experimental work on fatigue life with this material was performed, and good agreement was found with the results obtained in FE modeling. The number of cycles for fatigue crack propagation attains up to a maximum of 40% of the final fatigue lifetime with a typical value of 15% in many cases. This physically based two-scale technique significantly advances fatigue research, particularly in power plants, and paves the way for rapid and low-cost virtual material analysis and fatigue resistance analysis in the context of environmental fatigue applications.

Publisher

MDPI AG

Subject

General Materials Science,Metals and Alloys

Reference38 articles.

1. Quantifying Operational Lifetimes for Coal Power Plants Under the Paris Goals;Cui;Nat. Commun.,2019

2. Cycle Number Estimation Method on Fatigue Crack Initiation using Voronoi Tessellation and the Tanaka Mura Model;Rahim;J. Fail. Anal. Prev.,2023

3. Low Cycle Fatigue Behavior of Circumferentially Notched Specimens Made of Modified 9Cr-1Mo Steel at Elevated Temperature;Abarkan;Int. Rev. Appl. Sci. Eng.,2022

4. Speicher, M., Klenk, A., and Coleman, K. (2013, January 16–21). Creep-Fatigue Interactions in P91 Steel. Proceedings of the 13th International Conference on Fracture, Beijing, China.

5. Saxena, A., and Narasimhachary, S. (2018). Creep-Fatigue Crack Growth Testing of P91 Steel: Result of the Round Robin for Assessing ASTM Standard E-2760-10, EPRI.

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