Abstract
The metal additive manufacturing technology, with its savings in production time and the provision for expansive design capabilities has shown promise in the aerospace industry. Aerospace components have a critical need to be manufactured to endure in-service conditions, which includes durability when subject to variations in cyclic stress/strain loading histories including tensile mean stresses. Pulsating cyclic stresses in the tensile regime have proven detrimental to fatigue life, as they are prone to enhancing the rapid propagation of fatigue cracks. With this consideration, the current study has modeled the experimental fatigue performance of as-built additively manufactured stainless steel (SS) GP1 alloy, when subjected to progressive increases in cyclic strain range loads from Δε = 0.6% to Δε = 1.4%, and pulsating tension fatigue conditions. This is the first study to experimentally capture the cyclic stress–strain curve exhibited by stainless steel GP1 and to use the Chaboche model to model the hysteresis deformation response at varying strain amplitudes, providing a set of optimized Chaboche constants effective in capturing the kinematic/isotropic hardening behavior of this material under progressive amplitude fatigue and pulsating tension fatigue conditions.
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Acknowledgements
This work was supported by the National Science Foundation Graduate Research Fellowship Program under Grant No. 1144246, awarded to Sanna Siddiqui. The authors would like to thank Dr. Abiodun A. Fasoro for additively manufacturing the stainless steel GP1 specimens used in this study, which were developed using the EOS M280 system in the Manufacturing Engineering Department at Central State University. The authors would also like to acknowledge assistance in data analysis by Ms. Krystal Rivera, an undergraduate student at Florida Polytechnic University.
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Siddiqui, S.F., O’Nora, N. & Gordon, A.P. Modeling the Progressive Amplitude and Pulsating Tension Fatigue Response of Laser-Powder Bed Fusion Stainless Steel GP1. JOM 75, 1902–1914 (2023). https://doi.org/10.1007/s11837-022-05656-8
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DOI: https://doi.org/10.1007/s11837-022-05656-8