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Joint nonlinearity in a stiffened aluminium wingbox panel and what it requires of a reduced basis
and-sciencecomputational-engineeringfinancemathematical-physicsnumerical-analysissystems-and-control
A shell finite-element model of a stiffened aluminium wingbox panel, a laboratory structure shared by several experimental studies, is built with its plate-to-stiffener joints at the $78$ physical fastener positions and calibrated against measured modal data, a six-parameter sensitivity update of th
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