Shankar Sankararaman, You Ling, Christopher Shantz, and Sankaran Mahadevan
Publication Target:
IJPHM
Submission Type:
Full Paper
Supporting Agencies (optional):
NASA AMES Research Center, Federal Aviation Administration William J. Hughes Technical Center
This paper presents a methodology to quantify the uncertainty in fatigue crack growth prognosis, applied to structures with complicated geometry and subjected to variable amplitude multi-axial loading. Finite element analysis is used to address the complicated geometry and calculate the stress intensity factors. Multi-modal stress intensity factors due to multi-axial loading are combined to calculate an equivalent stress intensity factor using a characteristic plane approach. Crack growth under variable amplitude loading is modeled using a modified Paris law that includes retardation effects.
Publication Control Number:
001
Submission Keywords:
model-based methods
Fatigue Prognosis
Uncertainty Quantification
Natural Variability
Data Uncertainty
Model Error
Fracture Mechanics
Crack Growth
Submission Topic Areas:
Model-based methods for fault detection, diagnostics, and prognosis
Modeling and simulation
Structural health monitoring
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