Conference Presentation: A System for Simulation Governance of Engineered Repairs of Composite Aircraft Structures
Abstract: Modern military aircraft = composite skins + metallic sub-structure. Verification of structural integrity of standard repairs is costly, and requires structural and strength analysis. Traditional closed-form analysis techniques are unrepresentative and unsuitable, but construction of detailed finite element models requires Finite Element Analysis (FEA) expertise. Therefore, computational system with these requirements is needed to accelerate decision-making:
- Validated/certified methods
- Closed-form and FEA-based
- Readily employed
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