HAL (France)
open access
Automated lifetime Prediction of As-Manufactured Aerospace Turbine Blades : From Computed Tomography to Multi-physics Finite-Element Simulation through Functional Maps
High-pressure turbine blades have tight tolerances and complex, thin-walled features. This makes thermo-mechanical predictions highly sensitive to geometric variability induced by manufacturing. This thesis presents a digital twin workflow that uses X-ray computed tomography to capture real geometry
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