Fracture mechanics-based approach for anomaly size acceptability of additively manufactured metalsicaf2023 Tracking Number 133 Presentation: Session: Session 7: Fatigue crack growth and life prediction methodsĀ III Room: Theatre room: plenary Session start: 13:30 Tue 27 Jun 2023 Simone Romano simone.romano@avioaero.it Affifliation: GE Avio Andrew Perry andrew.c.perry1@ge.com Affifliation: GE Aerospace Francesco Sausto francesco.sausto@avioaero.it Affifliation: GE Avio Apostolos Karafillis apostolos.karafillis@ge.com Affifliation: GE Aerospace Topics: - Fatigue crack growth and life prediction methods (Genral Topics) Abstract: The traditional approach for quantifying material capability generally assumes that material properties in components are fully represented by test bar results. However, this assumption might not always be true for complex additively manufactured components, which may contain anomaly populations different than those expected based on relatively simple-geometry mechanical test coupons. In this work, we present a possible fracture mechanics-based approach for definition of anomaly size acceptability limits for AM materials, to augment the traditional building block of fatigue test-based material capability assessments. The fracture mechanics analysis is validated against fractography observations of tested bars and with fatigue tests on bars containing artificially notched coupons. |