Assembly-like FEM updating performs ~95% of solves on subassemblies for 28% lower workload proxy effort with fidelity within 1% of global updating on experimental flexible wing data.
Pontillo, High Aspect Ratio Wings on Commercial Aircraft: a Numerical and Experimental approach, Phd thesis, Centre for Aeronautics, Cranfield University (2020)
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A Paradigm Shift to Assembly-like Finite Element Model Updating
Assembly-like FEM updating performs ~95% of solves on subassemblies for 28% lower workload proxy effort with fidelity within 1% of global updating on experimental flexible wing data.