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Description
Damage Tolerance Assessments and Fracture processes of
Aerospace Materials
Madhav Baral, Ph.D. (PI)
Department of Mechanical Engineering
University of Kentucky - Paducah
ABSTRACT
Damages in aircraft structures can occur during manufacturing processes or during service. As a
result, structures must be designed to withstand service load and perform reliably throughout the
service life in the presence of a crack or damage. Assessing damage requires a deep understanding
of material behavior, fracture mechanics, and experimental characterization. The proposed
research activity aims to develop a methodology to assess the damage tolerance behavior and
fracture processes of aerospace materials through extensive experimental scheme employing
conventional and novel test designs. The mechanical properties of the material will be
characterized using tension, compression, and plane-strain experiments along major material
directions to assess the anisotropic mechanical behavior. The fracture behavior will be
characterized using a series of specialized tests and specimen geometries aimed to determine the
strain at fracture for different stress states. Likewise, the resistance of the material against cracking
will be characterized using fracture toughness and fatigue crack growth tests on specimens
extracted along major material directions. These experimentally determined parameters will enable
the development of material modeling framework that can predict the failure over a range of
loading conditions, and aid in the design, selection, and development of damage tolerant structures
for aerospace and space applications.
Status | Active |
---|---|
Effective start/end date | 7/1/23 → 12/31/24 |
Funding
- KY Economic Development Cab
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