Abstract
For accurate prediction of composite failure, microstructural variability must be considered. The distribution of epoxy stiffness and hardness were determined by nanoindentation and used in stochastic finite element modeling. Another key microstructural feature, fiber volume fraction variability, was determined by image processing of an SEM image. Stochastic failure analysis was implemented on a hexagonal fiber packing micromechanics model to predict the initiation of failure under multiaxial loadings. Three failure criteria were employed for characterization of failure: maximum stress, von Mises, and Christensen. Failure envelopes were developed for three different reliability levels. The results revealed that the variability in epoxy strength influence the failure behavior significantly, whereas, stiffness variability has minimal effect.
Original language | English (US) |
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Title of host publication | 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference |
Publisher | American Institute of Aeronautics and Astronautics Inc. |
ISBN (Electronic) | 9781624103421 |
State | Published - Jan 1 2015 |
Event | 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015 - Kissimmee, United States Duration: Jan 5 2015 → Jan 9 2015 |
Other
Other | 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015 |
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Country/Territory | United States |
City | Kissimmee |
Period | 1/5/15 → 1/9/15 |
All Science Journal Classification (ASJC) codes
- Civil and Structural Engineering
- Architecture
- Mechanics of Materials
- Building and Construction