Fatigue behavior of a 22Cr-20Ni-18Co-Fe alloy at elevated temperatures
Abstract
An experimental investigation was conducted on Haynes Alloy 556 to study the fatigue behavior of the material at elevated temperatures. Fatigue tests were run at constant temperatures ranging from room temperature to 871° C with strain ranges from 0.265 to 1.5 percent resulting in lives between 102 and 106 cycles. Cyclic deformation properties were evaluated based on the fatigue data. Three fatigue life models were evaluated for their ability to predict the isothermal fatigue lives of the material. These included the Ostergren, Frequency Separation and Stress-Strain-Time models. Strengths and weaknesses of each model are discussed based on the experimental results. © 1994 by ASME.
Publication Title
Journal of Engineering Materials and Technology, Transactions of the ASME
Recommended Citation
Krukemyer, T., Fatemi, A., & Swindeman, R. (1994). Fatigue behavior of a 22Cr-20Ni-18Co-Fe alloy at elevated temperatures. Journal of Engineering Materials and Technology, Transactions of the ASME, 116 (1), 54-61. https://doi.org/10.1115/1.2904255
