Electronic Theses and Dissertations
Date
2025
Document Type
Dissertation
Degree Name
Doctor of Philosophy
Department
Mechanical Engineering
Committee Chair
Ali Fatemi
Committee Member
Ali Fatemi
Committee Member
Gladius Lewis
Committee Member
John Williams
Committee Member
José Alexander Araújo
Committee Member
Yue Guan
Abstract
Fretting fatigue, a critical failure mechanism in structural assemblies, occurs due to small-amplitude relative motion between contacting surfaces under cyclic loading, significantly compromising fatigue life. Despite extensive studies, the understanding of coupled influences of mechanical, material, and environmental factors remains incomplete, motivating the need for integrated experimental and predictive modeling approaches. This dissertation first provides a comprehensive literature review and synthesis of experimental studies of key fretting fatigue parameters including contact pressure, slip amplitude, frequency, surface roughness, contact geometry, and environment. Then the fretting fatigue life modeling approaches used in the literature are reviewed and their strengths and limitations are discussed. A critical plane approach combining the Fatemi–Socie (FS) parameter with the Theory of Critical Distances (TCD) was selected and validated against extensive fretting fatigue literature data on aluminum and titanium alloys. The FS parameter accounts for the complex non-proportional multiaxial stresses, the interaction between tangential-to-normal stress, and the mean stress effects. TCD accounts for the steep gradients at contact interfaces. The life prediction framework utilized accurately predicted crack initiation at the trailing edge, crack orientations within the observed ranges, and fatigue lives within relatively narrow scatter bands. The study also presents a comprehensive analytical investigation into the fretting fatigue behavior of cold-sprayed ZE41A-T5 cast magnesium alloy, with particular emphasis on the influence of contact pressure, slip amplitude, and loading frequency. The data were generated with a custom-designed fretting fatigue test rig at the Army Research Laboratory enabling decoupled application of slip amplitude and axial loading to replicate service-relevant multiaxial stress states. A computationally efficient life prediction methodology was developed by integrating the stress concentration concept for local stresses used in the FS parameter. The modeling framework offers a practical and efficient tool for life prediction, reducing reliance on computationally intensive nonlinear analyses for each test scenario. The methodology used demonstrates strong correlation of the experimental data with observed fatigue life under diverse experimental fretting fatigue conditions, with all test data falling within ±1.5x scatter bands on life.
Library Comment
Dissertation or thesis originally submitted to ProQuest.
Notes
Open Access
Recommended Citation
Ghadar, Samira, "Experimental Investigation and Advanced Modeling of Fretting Fatigue: Analysis of Key Variables and Application of Critical Plane-Based Life Prediction Approach" (2025). Electronic Theses and Dissertations. 3916.
https://digitalcommons.memphis.edu/etd/3916
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Comments
Data is provided by the student.”