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This aper presents a novel framework for the measurement of large deformation of wings in flight by using strain data. The method is based on data obtained from a finite element model or a preliminary ground vibration test. The method is demonstrated both numerically and experimentally and is shown to be precise and robust.

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This page is a summary of: Large Deformation Shape Sensing Using a Nonlinear Strain to Displacement Method, AIAA Journal, June 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j061832.
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