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Shape sensing methods: Review and experimental comparison on a wing-shaped plate

Authors :
Marco Gherlone
Priscilla Cerracchio
Massimiliano Corrado Mattone
Source :
Progress in Aerospace Sciences. 99:14-26
Publication Year :
2018
Publisher :
Elsevier BV, 2018.

Abstract

Shape sensing, i.e., the reconstruction of the displacement field of a structure from some discrete surface strain measurements, is a fundamental capability for the structural health management of critical components. In this paper, a review of the shape sensing methodologies available in the open literature and of the different applications is provided. Then, for the first time, an experimental comparative study is presented among the main approaches in order to highlight their relative merits in presence of uncertainties affecting real applications. These approaches are, namely, the inverse Finite Element Method, the Modal Method and Ko's Displacement Theory. A brief description of these methods is followed by the presentation of the experimental test results. A cantilevered, wing-shaped aluminum plate is let deform under its own weight, leading to bending and twisting. Using the experimental strain measurements as input data, the deflection field of the plate is reconstructed using the three aforementioned approaches and compared with the actual measured deflection. The inverse Finite Element Method is proven to be slightly more accurate and particularly attractive because it is versatile with respect to the boundary conditions and it does not require any information about material properties and loading conditions.

Details

ISSN :
03760421
Volume :
99
Database :
OpenAIRE
Journal :
Progress in Aerospace Sciences
Accession number :
edsair.doi.dedup.....de74428d9e5d022b4050b39f7b0b966f
Full Text :
https://doi.org/10.1016/j.paerosci.2018.04.001