Hybrid Shell-Beam Inverse Finite Element Method for the Shape Sensing of Stiffened Thin-Walled Structures: Formulation and Experimental Validation on a Composite Wing-Shaped Panel

• Published in: Sensors (Basel, Switzerland) Vol. 23; no. 13; p. 5962
• Main Authors: Esposito, Marco, Roy, Rinto, Surace, Cecilia, Gherlone, Marco
• Format: Journal Article
• Language: English
• Published: Switzerland MDPI AG 27-06-2023; MDPI
• Subjects: Accuracy; carbon-epoxy panel; Composite wings; Deformation; Digital twins; Elastic deformation; Equipment and supplies; Fiber Optic Technology; Fiber optics; Finite Element Analysis; Finite element method; Inverse problems; Investigations; Kinematics; Load; Methods; mindlin plate; Sensors; Shape functions; shape sensing; structural health monitoring; Thin wall structures; timoshenko beam; Wing panels; fiber optics; inverse problem; shape sensing; structural health monitoring; timoshenko beam; mindlin plate; carbon-epoxy panel
• ISSN: 1424-8220; 1424-8220
• DOI: 10.3390/s23135962

This work presents a novel methodology for the accurate and efficient elastic deformation reconstruction of thin-walled and stiffened structures from discrete strains. It builds on the inverse finite element method (iFEM), a variationally-based shape-sensing approach that reconstructs structural displacements by matching a set of analytical and experimental strains in a least-squares sense. As iFEM employs the finite element framework to discretize the structural domain and as the displacements and strains are approximated using element shape functions, the kind of element used influences the accuracy and efficiency of the iFEM analysis. This problem is addressed in the present work through a novel discretization scheme that combines beam and shell inverse elements to develop an iFEM model of the structure. Such a hybrid discretization paradigm paves the way for more accurate shape-sensing of geometrically complex structures using fewer sensor measurements and lower computational effort than traditional approaches. The hybrid iFEM is experimentally demonstrated in this work for the shape sensing of bending and torsional deformations of a composite stiffened wing panel instrumented with strain rosettes and fiber-optic sensors. The experimental results are accurate, robust, and computationally efficient, demonstrating the potential of this hybrid scheme for developing an efficient digital twin for online structural monitoring and control.