Biaxial fatigue crack propagation in AL 7075-t6 alloy under the influence of mixed-mode overloads

Siddhant Datta, Aditi Chattopadhyay, Nagaraja Iyyer, Nam Phan

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Fatigue crack growth behavior of Al 7075-T6 alloy was investigated under in-plane biaxial fatigue loading with mixed-mode overloads. Cruciform geometry specimens were tested with specially programmed load spectra having single mixed-mode (mode I+II) overloads within a constant amplitude pure mode-I baseline load spectrum. The effects of mixed-mode overloads of different magnitudes on crack retardation behavior and crack growth micromechanisms were studied in detail by correlating the macroscale crack growth rates with fracture surface morphology through quantitative fractography. The retardation effects were found to increase with overload ratio and with the instantaneous fatigue crack at the instance of overload. Mode-mixity induced crack closure mechanisms played a dominant role in crack retardation for shorter cracks while mode-I plasticity induced crack closure was observed to be the dominant mechanism in the case of longer crack lengths.

Original languageEnglish (US)
Title of host publicationAIAA Scitech 2019 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105784
DOIs
StatePublished - Jan 1 2019
EventAIAA Scitech Forum, 2019 - San Diego, United States
Duration: Jan 7 2019Jan 11 2019

Publication series

NameAIAA Scitech 2019 Forum

Conference

ConferenceAIAA Scitech Forum, 2019
CountryUnited States
CitySan Diego
Period1/7/191/11/19

ASJC Scopus subject areas

  • Aerospace Engineering

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    Datta, S., Chattopadhyay, A., Iyyer, N., & Phan, N. (2019). Biaxial fatigue crack propagation in AL 7075-t6 alloy under the influence of mixed-mode overloads. In AIAA Scitech 2019 Forum (AIAA Scitech 2019 Forum). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2019-0413