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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The capabilities available with BAMF, AFGROW and StressCheck® are highly advanced and offer significant potential to achieve the high-level goal of TITANS –to reduce the need to conduct expensive and time consuming physical tests and to rely more on simulation.
Dr. Kevin WalkerDefence Science and Technology Group – Melbourne, Australia