SBIR/STTR Research Award
Failure Initiation Prediction for Reliability-Based Design of Hybrid Composite Materials
Award amount
$99,991Program and phase
STTR · Phase IAward year
2009Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- Firehole Technologies, Inc.
- Proposal award date
- 2008-08-01
- Contract end date
- 2009-04-01
- UEI
- Not reported
- Solicitation number
- 2008.A
- Topic code
- AF08-T025
Research abstract
The opportunity identified here is to expand the capabilities of Multicontinuum Technology (MCT) for prediction of failure initiation in complex (hybrid) composites. A successful Phase 1 project will demonstrate good correlation of MCT variables with initial failure in composites with complex multiscale reinforcement architectures. A Phase 2 project would refine the predictive capabilities, embody the capabilities in user friendly software, and construct an application analysis environment within a probabilistic framework. The specific opportunity is to develop and demonstrate theory and associate computational tools that will be highly effective for structural analysis and initial failure prediction for complex hybrid composite material systems. The MCT approach is a computationally inexpensive finite element based multiscale approach that decomposes the complex heterogeneous material response into fundamental variables that directly relate to actual physical damage/failure at the microstructural level. MCT failure predictions will be compared with experimental data found in the literature for a triaxial braid reinforced material.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Failure Initiation Prediction for Reliability-Based Design of Hybrid Composite Materials
- Failure Initiation Predictors for Reliability-Based Design of Hybrid Composite Materials
- Failure Initiation Predictors for Reliability-Based Design of Hybrid Composite Materials
- MMF-based Failure Initiation and Progression for Hybrid Composite Materials