scholarly journals Final Report for Project 13-4791: New Mechanistic Models of Creep-Fatigue Crack Growth Interactions for Advanced High Temperature Reactor Components

2018 ◽  
Author(s):  
Jamie J Kruzic ◽  
Thomas Siegmund ◽  
Vikas Tomar
Author(s):  
R. A. Ainsworth ◽  
P. J. Budden ◽  
D. W. Dean ◽  
M. J. H. Fox ◽  
M. P. O’Donnell ◽  
...  

Parts of the R5 high temperature assessment procedures address creep and creep-fatigue crack growth. The procedures were developed some years ago as separate approaches for creep crack growth (R5 Volume 4) and creep-fatigue crack growth (R5 Volume 5). A major revision to these procedures has recently been completed. This unifies the separate approaches into a single procedure for creep-fatigue crack growth (R5 Volume 4/5). The revision restructures the procedure for easier application and includes a number of technical developments, including criteria for deciding when creep-fatigue interactions are important. This paper describes in outline the new R5 creep-fatigue crack growth procedure.


2019 ◽  
Author(s):  
Afsaneh Rabiei ◽  
Paul Bowen ◽  
Amrita Lall ◽  
Siddhartha Sarkar ◽  
Swathi Upadhyay ◽  
...  

2019 ◽  
Author(s):  
Gabriel Potirniche ◽  
Robert Stephens ◽  
Indrajit Charit ◽  
Nicholas Shaber ◽  
Jose Ramirez ◽  
...  

2010 ◽  
Vol 4 (9) ◽  
pp. 1410-1426 ◽  
Author(s):  
Tae Wuk WOO ◽  
Masao SAKANE ◽  
Kwang Soo KIM ◽  
Kaoru KOBAYASHI ◽  
Hyun Chul PARK

Materials ◽  
2022 ◽  
Vol 15 (2) ◽  
pp. 651
Author(s):  
Jianxing Mao ◽  
Zhixing Xiao ◽  
Dianyin Hu ◽  
Xiaojun Guo ◽  
Rongqiao Wang

The creep-fatigue crack growth problem remains challenging since materials exhibit different linear and nonlinear behaviors depending on the environmental and loading conditions. In this paper, we systematically carried out a series of creep-fatigue crack growth experiments to evaluate the influence from temperature, stress ratio, and dwell time for the nickel-based superalloy GH4720Li. A transition from coupled fatigue-dominated fracture to creep-dominated fracture was observed with the increase of dwell time at 600 °C, while only the creep-dominated fracture existed at 700 °C, regardless of the dwell time. A concise binomial crack growth model was constructed on the basis of existing phenomenal models, where the linear terms are included to express the behavior under pure creep loading, and the nonlinear terms were introduced to represent the behavior near the fracture toughness and during the creep-fatigue interaction. Through the model implementation and validation of the proposed model, the correlation coefficient is higher than 0.9 on ten out of twelve sets of experimental data, revealing the accuracy of the proposed model. This work contributes to an enrichment of creep-fatigue crack growth data in the typical nickel-based superalloy at elevated temperatures and could be referable in the modeling for damage tolerance assessment of turbine disks.


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